diff --git a/examples/scripts/ssbj.py b/examples/scripts/ssbj.py
index 4b8f46b10d267ef886a9c9e613dc25903f3e5a68..ba3d9ffa5bcf2126e7f8912638a0377500e2ca44 100644
--- a/examples/scripts/ssbj.py
+++ b/examples/scripts/ssbj.py
@@ -25,11 +25,11 @@ cmdows_dir = 'ssbj/CMDOWS'
kdms_dir = 'ssbj/KDMS'
vistoms_dir = 'ssbj/VISTOMS'
-print 'Loading repository connectivity graph...'
+print('Loading repository connectivity graph...')
rcg = load(os.path.join(kb_dir, 'ssbj', '__cmdows__SSBJ.xml'))
-print 'Scripting RCG...'
+print('Scripting RCG...')
# A name and a description are added to the graph
rcg.graph['name'] = 'RCG'
@@ -79,7 +79,7 @@ rcg.add_mathematical_function([[item[0], item[1]] for item in zip(prop_nodes, pr
# Add the objective
R = [node for node in rcg.find_all_nodes(category='variable') if node.endswith('/R')]
-R_label = dpdx[0].split('/')[-1]
+R_label = R[0].split('/')[-1]
f_R = '/data_schema/mdo_data/objectives/R'
rcg.add_mathematical_function([[R[0], R_label]], 'F[R]', [[f_R, '-{}'.format(R_label), 'Python']])
@@ -165,7 +165,7 @@ fpg.save('FPG_' + architecture_type, file_type='cmdows', destination_folder=cmdo
integrity=True)
for mdao_definition in mdao_definitions:
- print 'Scripting ' + str(mdao_definition) + '...'
+ print('Scripting ' + str(mdao_definition) + '...')
# Change the problem formulation of the FPG based on the MDAO definition
fpg.add_problem_formulation(mdao_definition, function_order)
diff --git a/examples/scripts/ssbj/(X)DSM/FPG_MDA.pdf b/examples/scripts/ssbj/(X)DSM/FPG_MDA.pdf
index d50170b2a35d2bdc4c118e5771efc2babddaf541..6f0444f48828ff6e8f57126b23395483b9c42d1f 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/FPG_MDO.pdf b/examples/scripts/ssbj/(X)DSM/FPG_MDO.pdf
index 1b45661fbb87afb7347d33c24da8be3e290c6459..44c6b2ee8b19872e5e899190f7ae20fd1dedcbc5 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_BLISS-2000.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_BLISS-2000.pdf
index ad8fc5342dd9cae9e7ab0ae8c858e245a95371f6..204916a39c25412e30109b3b08b3e718d8e0b57c 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_CO.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_CO.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_IDF.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_IDF.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_MDF-GS.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_MDF-GS.pdf
index c5b516fc1ad46d7a09c623038c90d9248e7d10ff..0ca478c64392d9331796b508082da1bfd1d07380 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_MDF-J.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_MDF-J.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-GS.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-GS-CT.pdf
similarity index 78%
rename from examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-GS.pdf
rename to examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-GS-CT.pdf
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new file mode 100644
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new file mode 100644
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new file mode 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-J.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-J-CT.pdf
similarity index 78%
rename from examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-J.pdf
rename to examples/scripts/ssbj/(X)DSM/Mdao_converged-DOE-J-CT.pdf
index e67c9b3e994cb6258c32d62076522b5e3358c1d7..3277e4209a9ec8fe74945a319cf018ceb7bbc03b 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_converged-MDA-GS.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_converged-MDA-GS.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-GS.pdf b/examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-GS-CT.pdf
similarity index 88%
rename from examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-GS.pdf
rename to examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-GS-CT.pdf
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similarity index 88%
rename from examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-J.pdf
rename to examples/scripts/ssbj/(X)DSM/Mdao_unconverged-DOE-J-CT.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/RCG_basic.pdf b/examples/scripts/ssbj/(X)DSM/RCG_basic.pdf
index 633577d3fe3648d5e42978cff42e7a130bf2c24d..65ba55483abcdc12e335c1bf594ef569c522e8cb 100644
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diff --git a/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf b/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf
index 392bd30adc5d5198572d8e983441d39f7e3b4b49..83a99c4a4e80625505a16a9ffb19f9bf26942a05 100644
Binary files a/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf and b/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf differ
diff --git a/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml b/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
index b12f64be37371d8bee0d78e72d2fb63d716f0b68..31159a8f1f8b15122cb2e7af7893c868bfbda329 100644
--- a/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
+++ b/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>FPG CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a fundamental problem graph (FPG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -222,14 +222,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -498,9 +498,9 @@
<label>Lambda</label>
</parameter>
</parameters>
- <problemDefinition uID="unconverged-MDAGauss-Seidel">
+ <problemDefinition uID="converged-DOEGauss-Seidel">
<problemFormulation>
- <mdaoArchitecture>unconverged-MDA</mdaoArchitecture>
+ <mdaoArchitecture>converged-DOE</mdaoArchitecture>
<convergerType>Gauss-Seidel</convergerType>
<executableBlocksOrder>
<executableBlock position="1">Structures[main][1][1.0]</executableBlock>
@@ -513,11 +513,240 @@
<executableBlock position="8">C[prop]</executableBlock>
<executableBlock position="9">F[R]</executableBlock>
</executableBlocksOrder>
- <allowUnconvergedCouplings>true</allowUnconvergedCouplings>
+ <allowUnconvergedCouplings>false</allowUnconvergedCouplings>
+ <doeSettings>
+ <doeMethod>Monte Carlo design</doeMethod>
+ <doeRuns>10</doeRuns>
+ </doeSettings>
</problemFormulation>
<problemRoles>
<parameters>
+ <designVariables>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ <nominalValue>0.25</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>0.4</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.116666666667</sample>
+ <sample position="3">0.133333333333</sample>
+ <sample position="4">0.15</sample>
+ <sample position="5">0.166666666667</sample>
+ <sample position="6">0.183333333333</sample>
+ <sample position="7">0.2</sample>
+ <sample position="8">0.216666666667</sample>
+ <sample position="9">0.233333333333</sample>
+ <sample position="10">0.25</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/T">
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ <nominalValue>0.55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>1.0</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.15</sample>
+ <sample position="3">0.2</sample>
+ <sample position="4">0.25</sample>
+ <sample position="5">0.3</sample>
+ <sample position="6">0.35</sample>
+ <sample position="7">0.4</sample>
+ <sample position="8">0.45</sample>
+ <sample position="9">0.5</sample>
+ <sample position="10">0.55</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <nominalValue>5.5</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>2.5</minimum>
+ <maximum>8.5</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">2.5</sample>
+ <sample position="2">2.83333333333</sample>
+ <sample position="3">3.16666666667</sample>
+ <sample position="4">3.5</sample>
+ <sample position="5">3.83333333333</sample>
+ <sample position="6">4.16666666667</sample>
+ <sample position="7">4.5</sample>
+ <sample position="8">4.83333333333</sample>
+ <sample position="9">5.16666666667</sample>
+ <sample position="10">5.5</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <nominalValue>1000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>500</minimum>
+ <maximum>1500</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">500.0</sample>
+ <sample position="2">555.555555556</sample>
+ <sample position="3">611.111111111</sample>
+ <sample position="4">666.666666667</sample>
+ <sample position="5">722.222222222</sample>
+ <sample position="6">777.777777778</sample>
+ <sample position="7">833.333333333</sample>
+ <sample position="8">888.888888889</sample>
+ <sample position="9">944.444444444</sample>
+ <sample position="10">1000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <nominalValue>0.05</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.01</minimum>
+ <maximum>0.09</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.01</sample>
+ <sample position="2">0.0144444444444</sample>
+ <sample position="3">0.0188888888889</sample>
+ <sample position="4">0.0233333333333</sample>
+ <sample position="5">0.0277777777778</sample>
+ <sample position="6">0.0322222222222</sample>
+ <sample position="7">0.0366666666667</sample>
+ <sample position="8">0.0411111111111</sample>
+ <sample position="9">0.0455555555556</sample>
+ <sample position="10">0.05</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/h">
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <nominalValue>45000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>30000</minimum>
+ <maximum>60000</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">30000.0</sample>
+ <sample position="2">31666.6666667</sample>
+ <sample position="3">33333.3333333</sample>
+ <sample position="4">35000.0</sample>
+ <sample position="5">36666.6666667</sample>
+ <sample position="6">38333.3333333</sample>
+ <sample position="7">40000.0</sample>
+ <sample position="8">41666.6666667</sample>
+ <sample position="9">43333.3333333</sample>
+ <sample position="10">45000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/M">
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <nominalValue>1.6</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>1.4</minimum>
+ <maximum>1.8</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">1.4</sample>
+ <sample position="2">1.42222222222</sample>
+ <sample position="3">1.44444444444</sample>
+ <sample position="4">1.46666666667</sample>
+ <sample position="5">1.48888888889</sample>
+ <sample position="6">1.51111111111</sample>
+ <sample position="7">1.53333333333</sample>
+ <sample position="8">1.55555555556</sample>
+ <sample position="9">1.57777777778</sample>
+ <sample position="10">1.6</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <nominalValue>55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>40</minimum>
+ <maximum>70</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">40.0</sample>
+ <sample position="2">41.6666666667</sample>
+ <sample position="3">43.3333333333</sample>
+ <sample position="4">45.0</sample>
+ <sample position="5">46.6666666667</sample>
+ <sample position="6">48.3333333333</sample>
+ <sample position="7">50.0</sample>
+ <sample position="8">51.6666666667</sample>
+ <sample position="9">53.3333333333</sample>
+ <sample position="10">55.0</sample>
+ </samples>
+ </designVariable>
+ </designVariables>
<stateVariables>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/dpdx">
<parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
</stateVariable>
diff --git a/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml b/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
index b2eee607c0da338b12e93b14cb9abed759ed360e..a19a4a52168218f592196ea9ac3d00c2d52a51a9 100644
--- a/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
+++ b/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>FPG CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a fundamental problem graph (FPG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -222,14 +222,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml b/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
index f363399d6e873396fac6bd954477ccb05436b2af..ac0059b8f87ef5378ad0afbd2536e21c17ab50d9 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-20T16:50:52.734083</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-20T16:50:52.734083</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -849,14 +849,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
<output>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml b/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
index fb286f9cc62c92bdf1d62fbecb9564b950f3a112..20c88ccfb29cf4b66bf08cda2128b178a6018cae 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -222,14 +222,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
<output>
@@ -259,27 +259,6 @@
</output>
</outputs>
</mathematicalFunction>
- <mathematicalFunction uID="C[dpdx]">
- <label>C[dpdx]</label>
- <inputs>
- <input>
- <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
- <equationLabel>dpdx</equationLabel>
- </input>
- </inputs>
- <outputs>
- <output>
- <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/dpdx</parameterUID>
- <equations uID="C[dpdx]_equation">
- <equation language="Python">dpdx/1.0</equation>
- </equations>
- </output>
- <output>
- <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
- <equationsUID>C[dpdx]_equation</equationsUID>
- </output>
- </outputs>
- </mathematicalFunction>
<mathematicalFunction uID="C[prop]">
<label>C[prop]</label>
<inputs>
@@ -329,6 +308,165 @@
</output>
</outputs>
</mathematicalFunction>
+ <mathematicalFunction uID="__J2__">
+ <label>J2</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ <equationLabel>x4_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ <equationLabel>x2_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ <equationLabel>x1_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <equationLabel>x0_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/h__i2</parameterUID>
+ <equationLabel>x0_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <equationLabel>x3_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M__i2</parameterUID>
+ <equationLabel>x3_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</parameterUID>
+ <equationLabel>x1_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/SFC</parameterUID>
+ <equationLabel>x2_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ <equationLabel>x4_0</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/distributedArchitectures/group2/objective</parameterUID>
+ <equations uID="__J2___equation">
+ <equation language="Python">(x0_1-x0_0)**2+(x1_1-x1_0)**2+(x2_1-x2_0)**2+(x3_1-x3_0)**2+(x4_1-x4_0)**2</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group2/objective</parameterUID>
+ <equationsUID>__J2___equation</equationsUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group2/objective</parameterUID>
+ <equationsUID>__J2___equation</equationsUID>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="__J0__">
+ <label>J0</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR</parameterUID>
+ <equationLabel>x3_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WF</parameterUID>
+ <equationLabel>x6_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <equationLabel>x2_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Sref</parameterUID>
+ <equationLabel>x2_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <equationLabel>x3_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ <equationLabel>x4_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta</parameterUID>
+ <equationLabel>x5_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <equationLabel>x0_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/tc</parameterUID>
+ <equationLabel>x0_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <equationLabel>x1_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WT</parameterUID>
+ <equationLabel>x4_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ <equationLabel>x5_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda</parameterUID>
+ <equationLabel>x1_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ <equationLabel>x6_0</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group0/objective</parameterUID>
+ <equations uID="__J0___equation">
+ <equation language="Python">(x0_1-x0_0)**2+(x1_1-x1_0)**2+(x2_1-x2_0)**2+(x3_1-x3_0)**2+(x4_1-x4_0)**2+(x5_1-x5_0)**2+(x6_1-x6_0)**2</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group0/objective</parameterUID>
+ <equationsUID>__J0___equation</equationsUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/distributedArchitectures/group0/objective</parameterUID>
+ <equationsUID>__J0___equation</equationsUID>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[dpdx]">
+ <label>C[dpdx]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ <equationLabel>dpdx</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/dpdx</parameterUID>
+ <equations uID="C[dpdx]_equation">
+ <equation language="Python">dpdx/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ <equationsUID>C[dpdx]_equation</equationsUID>
+ </output>
+ </outputs>
+ </mathematicalFunction>
<mathematicalFunction uID="C[sigmas]">
<label>C[sigmas]</label>
<inputs>
@@ -406,6 +544,99 @@
</output>
</outputs>
</mathematicalFunction>
+ <mathematicalFunction uID="__J1__">
+ <label>J1</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</parameterUID>
+ <equationLabel>x6_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <equationLabel>x1_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/tc__i2</parameterUID>
+ <equationLabel>x0_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <equationLabel>x4_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/D</parameterUID>
+ <equationLabel>x8_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/h</parameterUID>
+ <equationLabel>x1_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR__i2</parameterUID>
+ <equationLabel>x5_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M</parameterUID>
+ <equationLabel>x2_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <equationLabel>x0_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/L</parameterUID>
+ <equationLabel>x6_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Sref__i2</parameterUID>
+ <equationLabel>x4_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda__i2</parameterUID>
+ <equationLabel>x3_1</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <equationLabel>x2_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <equationLabel>x3_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ <equationLabel>x7_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ <equationLabel>x8_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <equationLabel>x5_0</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/fin</parameterUID>
+ <equationLabel>x7_1</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group1/objective</parameterUID>
+ <equations uID="__J1___equation">
+ <equation language="Python">(x0_1-x0_0)**2+(x1_1-x1_0)**2+(x2_1-x2_0)**2+(x3_1-x3_0)**2+(x4_1-x4_0)**2+(x5_1-x5_0)**2+(x6_1-x6_0)**2+(x7_1-x7_0)**2+(x8_1-x8_0)**2</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group1/objective</parameterUID>
+ <equationsUID>__J1___equation</equationsUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/distributedArchitectures/group1/objective</parameterUID>
+ <equationsUID>__J1___equation</equationsUID>
+ </output>
+ </outputs>
+ </mathematicalFunction>
</mathematicalFunctions>
</executableBlocks>
<parameters>
@@ -2788,6 +3019,14 @@
<optimizers>
<optimizer uID="Sys-Optimizer">
<label>Sys-OPT</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</designVariableUID>
@@ -2854,6 +3093,14 @@
</optimizer>
<optimizer uID="Sub-Optimizer-0">
<label>Sub-OPT-0</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR</designVariableUID>
@@ -2902,6 +3149,14 @@
</optimizer>
<optimizer uID="Sub-Optimizer-1">
<label>Sub-OPT-1</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/tc__i2</designVariableUID>
@@ -2938,6 +3193,14 @@
</optimizer>
<optimizer uID="Sub-Optimizer-2">
<label>Sub-OPT-2</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M__i2</designVariableUID>
@@ -2967,17 +3230,17 @@
</constraintVariables>
</optimizer>
</optimizers>
- <consistencyConstraintFunctions>
- <consistencyConstraintFunction uID="__J2__">
- <label>J2</label>
- </consistencyConstraintFunction>
- <consistencyConstraintFunction uID="__J0__">
- <label>J0</label>
- </consistencyConstraintFunction>
- <consistencyConstraintFunction uID="__J1__">
- <label>J1</label>
- </consistencyConstraintFunction>
- </consistencyConstraintFunctions>
+ <preCouplingAnalyses>
+ <preCouplingAnalysis>
+ <relatedExecutableBlockUID>__J2__</relatedExecutableBlockUID>
+ </preCouplingAnalysis>
+ <preCouplingAnalysis>
+ <relatedExecutableBlockUID>__J0__</relatedExecutableBlockUID>
+ </preCouplingAnalysis>
+ <preCouplingAnalysis>
+ <relatedExecutableBlockUID>__J1__</relatedExecutableBlockUID>
+ </preCouplingAnalysis>
+ </preCouplingAnalyses>
<coupledAnalyses>
<coupledAnalysis>
<relatedExecutableBlockUID>Structures[main][1][1.0]</relatedExecutableBlockUID>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml b/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
index 05f4db079c0cea68a95068e31e456737b0b4f192..8d5611cd47c2e0824ecee212db87813f0e7c32c8 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -240,14 +240,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
<output>
@@ -2239,6 +2239,14 @@
<optimizers>
<optimizer uID="Optimizer">
<label>OPT</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
index 3b840db8eb6ce4299729dae323d52a012357748d..cf8aa2e5986a67e0e8963ba2b3060ee877994f4a 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -231,14 +231,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
<output>
@@ -1854,6 +1854,14 @@
<optimizers>
<optimizer uID="Optimizer">
<label>OPT</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
@@ -1928,6 +1936,12 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<coupledAnalyses>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
index e3f547463ce61ec3b75ad54fc0d8a376be46d8bd..b4fa2bd8feaf1d762ff873931b2da3699bbe46e3 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -240,14 +240,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
<output>
@@ -1981,6 +1981,14 @@
<optimizers>
<optimizer uID="Optimizer">
<label>OPT</label>
+ <settings>
+ <maximum_iterations>1000</maximum_iterations>
+ <algorithm>Dakota Quasi-Newton method</algorithm>
+ <apply_scaling>True</apply_scaling>
+ <maximum_function_evaluations>1000</maximum_function_evaluations>
+ <constraint_tolerance>0.0001</constraint_tolerance>
+ <convergence_tolerance>0.0001</convergence_tolerance>
+ </settings>
<designVariables>
<designVariable>
<designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
@@ -2055,6 +2063,12 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<coupledAnalyses>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
similarity index 97%
rename from examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS.xml
rename to examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
index ba9651df52f95da7638aa6b87a30b42584fdc0ef..2d2fe996d16b86550b57bf81e67102d455b29541 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -130,9 +130,15 @@
</input>
</inputs>
<outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/reference/ESF</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/reference/Temp</parameterUID>
</output>
@@ -142,9 +148,6 @@
<output>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
</output>
- <output>
- <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
- </output>
</outputs>
</designCompetence>
<designCompetence uID="Structures[main][1][1.0]">
@@ -222,14 +225,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -374,9 +377,6 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
- <parameter uID="/data_schema/aircraft/weight/WE">
- <label>WE</label>
- </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -476,6 +476,9 @@
<parameter uID="/data_schema/aircraft/weight/WT">
<label>WT</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/geometry/AR">
<label>AR</label>
</parameter>
@@ -776,6 +779,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/dpdx">
<parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
</stateVariables>
</parameters>
<executableBlocks>
@@ -798,7 +804,7 @@
<workflow>
<problemDefinitionUID>converged-DOEGauss-Seidel</problemDefinitionUID>
<dataGraph>
- <name>XDSM - converged-DOE-GS - Mdao</name>
+ <name>XDSM - converged-DOE-GS-CT - Mdao</name>
<edges>
<edge>
<fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</fromParameterUID>
@@ -816,6 +822,10 @@
<fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
<toExecutableBlockUID>DOE</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
@@ -880,6 +890,10 @@
<fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>Converger</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
@@ -904,6 +918,10 @@
<fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
<toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</toParameterUID>
@@ -1074,51 +1092,51 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/h</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
@@ -1130,24 +1148,28 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/M</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
@@ -1236,25 +1258,29 @@
<fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
<toExecutableBlockUID>Coordinator</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/ESF</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
+ <toParameterUID>/data_schema/reference/Temp</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Converger</fromExecutableBlockUID>
@@ -1415,7 +1441,7 @@
</edges>
</dataGraph>
<processGraph>
- <name>XDSM - converged-DOE-GS - Mdao</name>
+ <name>XDSM - converged-DOE-GS-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -1620,6 +1646,12 @@
<label>L^{c0}</label>
</initialGuessCouplingVariable>
</initialGuessCouplingVariables>
+ <finalCouplingVariables>
+ <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{*}</label>
+ </finalCouplingVariable>
+ </finalCouplingVariables>
<couplingCopyVariables>
<couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE">
<relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
@@ -1677,6 +1709,10 @@
</doeInputSampleList>
</doeInputSampleLists>
<doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
<doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT">
<relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</relatedParameterUID>
<label>DOE_DT_{out}</label>
@@ -1732,12 +1768,19 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<does>
<doe uID="DOE">
<label>DOE</label>
<settings>
+ <doeMethod>Custom design table</doeMethod>
<doeTable>
<tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
<tableElement experimentID="0">0.1</tableElement>
@@ -1860,7 +1903,6 @@
<tableElement experimentID="9">1.6</tableElement>
</tableRow>
</doeTable>
- <doeMethod>Custom design table</doeMethod>
</settings>
<designVariables>
<designVariable>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml
new file mode 100644
index 0000000000000000000000000000000000000000..fa391d6b91236f12a21f5862b060d054e019f270
--- /dev/null
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml
@@ -0,0 +1,1854 @@
+<?xml version='1.0' encoding='UTF-8'?>
+<cmdows xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="https://bitbucket.org/imcovangent/cmdows/raw/master/schema/0.7/cmdows.xsd">
+ <header>
+ <creator>Imco van Gent</creator>
+ <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ <updates>
+ <update>
+ <modification>KADMOS export of a mdao data graph (MDG).</modification>
+ <creator>Imco van Gent</creator>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ </update>
+ </updates>
+ </header>
+ <executableBlocks>
+ <designCompetences>
+ <designCompetence uID="Performance[main][1][1.0]">
+ <ID>Performance</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Performance</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Aerodynamics[main][1][1.0]">
+ <ID>Aerodynamics</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Aerodynamics</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/CDmin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/L</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Propulsion[main][1][1.0]">
+ <ID>Propulsion</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Propulsion</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WBE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Structures[main][1][1.0]">
+ <ID>Structures</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Structures</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Nz</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WFO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ </designCompetences>
+ <mathematicalFunctions>
+ <mathematicalFunction uID="F[R]">
+ <label>F[R]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ <equationLabel>R</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ <equations uID="F[R]_equation">
+ <equation language="Python">-R</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[Theta]">
+ <label>C[Theta]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ <equationLabel>Theta</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ <equations uID="C[Theta]_equation">
+ <equation language="Python">Theta/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[dpdx]">
+ <label>C[dpdx]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ <equationLabel>dpdx</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ <equations uID="C[dpdx]_equation">
+ <equation language="Python">dpdx/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[prop]">
+ <label>C[prop]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ <equationLabel>ESF</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ <equationLabel>Temp</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ <equationLabel>DT</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ <equations uID="C[prop]_equation">
+ <equation language="Python">ESF/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ <equations uID="C[prop]_equation_1">
+ <equation language="Python">DT/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ <equations uID="C[prop]_equation_2">
+ <equation language="Python">Temp/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[sigmas]">
+ <label>C[sigmas]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ <equationLabel>sigma5</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ <equationLabel>sigma4</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ <equationLabel>sigma3</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ <equationLabel>sigma2</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ <equationLabel>sigma1</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ <equations uID="C[sigmas]_equation">
+ <equation language="Python">sigma4/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ <equations uID="C[sigmas]_equation_1">
+ <equation language="Python">sigma5/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ <equations uID="C[sigmas]_equation_2">
+ <equation language="Python">sigma1/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ <equations uID="C[sigmas]_equation_3">
+ <equation language="Python">sigma2/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ <equations uID="C[sigmas]_equation_4">
+ <equation language="Python">sigma3/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ </mathematicalFunctions>
+ </executableBlocks>
+ <parameters>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WO">
+ <label>WO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WF">
+ <label>WF</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/L">
+ <label>L</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/D">
+ <label>D</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/fin">
+ <label>fin</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/T">
+ <label>T</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Cf">
+ <label>Cf</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Nz">
+ <label>Nz</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/lambda">
+ <label>lambda</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/objectives/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/SFC">
+ <label>SFC</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WFO">
+ <label>WFO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/CDmin">
+ <label>CDmin</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/section">
+ <label>section</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WBE">
+ <label>WBE</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WT">
+ <label>WT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/AR">
+ <label>AR</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/tc">
+ <label>tc</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Sref">
+ <label>Sref</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/h">
+ <label>h</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/M">
+ <label>M</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Lambda">
+ <label>Lambda</label>
+ </parameter>
+ </parameters>
+ <problemDefinition uID="converged-DOEGauss-Seidel">
+ <problemFormulation>
+ <mdaoArchitecture>converged-DOE</mdaoArchitecture>
+ <convergerType>Gauss-Seidel</convergerType>
+ <executableBlocksOrder>
+ <executableBlock position="1">Structures[main][1][1.0]</executableBlock>
+ <executableBlock position="2">Aerodynamics[main][1][1.0]</executableBlock>
+ <executableBlock position="3">Propulsion[main][1][1.0]</executableBlock>
+ <executableBlock position="4">Performance[main][1][1.0]</executableBlock>
+ <executableBlock position="5">C[sigmas]</executableBlock>
+ <executableBlock position="6">C[Theta]</executableBlock>
+ <executableBlock position="7">C[dpdx]</executableBlock>
+ <executableBlock position="8">C[prop]</executableBlock>
+ <executableBlock position="9">F[R]</executableBlock>
+ </executableBlocksOrder>
+ <allowUnconvergedCouplings>false</allowUnconvergedCouplings>
+ <doeSettings>
+ <doeMethod>Full factorial design</doeMethod>
+ <doeRuns>2</doeRuns>
+ </doeSettings>
+ </problemFormulation>
+ <problemRoles>
+ <parameters>
+ <designVariables>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/T">
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ <nominalValue>0.55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>1.0</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.15</sample>
+ <sample position="3">0.2</sample>
+ <sample position="4">0.25</sample>
+ <sample position="5">0.3</sample>
+ <sample position="6">0.35</sample>
+ <sample position="7">0.4</sample>
+ <sample position="8">0.45</sample>
+ <sample position="9">0.5</sample>
+ <sample position="10">0.55</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
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+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ <nominalValue>0.25</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>0.4</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.116666666667</sample>
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+ <sample position="4">0.15</sample>
+ <sample position="5">0.166666666667</sample>
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+ <sample position="7">0.2</sample>
+ <sample position="8">0.216666666667</sample>
+ <sample position="9">0.233333333333</sample>
+ <sample position="10">0.25</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
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+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <nominalValue>5.5</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>2.5</minimum>
+ <maximum>8.5</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">2.5</sample>
+ <sample position="2">2.83333333333</sample>
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+ <sample position="5">3.83333333333</sample>
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+ <sample position="8">4.83333333333</sample>
+ <sample position="9">5.16666666667</sample>
+ <sample position="10">5.5</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <nominalValue>0.05</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.01</minimum>
+ <maximum>0.09</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.01</sample>
+ <sample position="2">0.0144444444444</sample>
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+ <sample position="4">0.0233333333333</sample>
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+ <sample position="9">0.0455555555556</sample>
+ <sample position="10">0.05</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <nominalValue>1000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>500</minimum>
+ <maximum>1500</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">500.0</sample>
+ <sample position="2">555.555555556</sample>
+ <sample position="3">611.111111111</sample>
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+ <sample position="10">1000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/h">
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <nominalValue>45000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>30000</minimum>
+ <maximum>60000</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">30000.0</sample>
+ <sample position="2">31666.6666667</sample>
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+ <sample position="4">35000.0</sample>
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+ <sample position="10">45000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/M">
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <nominalValue>1.6</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>1.4</minimum>
+ <maximum>1.8</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">1.4</sample>
+ <sample position="2">1.42222222222</sample>
+ <sample position="3">1.44444444444</sample>
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+ <sample position="8">1.55555555556</sample>
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+ <sample position="10">1.6</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <nominalValue>55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>40</minimum>
+ <maximum>70</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">40.0</sample>
+ <sample position="2">41.6666666667</sample>
+ <sample position="3">43.3333333333</sample>
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+ <sample position="8">51.6666666667</sample>
+ <sample position="9">53.3333333333</sample>
+ <sample position="10">55.0</sample>
+ </samples>
+ </designVariable>
+ </designVariables>
+ <stateVariables>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/DT">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/Theta">
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/Temp">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/dpdx">
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
+ </stateVariables>
+ </parameters>
+ <executableBlocks>
+ <coupledBlocks>
+ <coupledBlock>Structures[main][1][1.0]</coupledBlock>
+ <coupledBlock>Aerodynamics[main][1][1.0]</coupledBlock>
+ <coupledBlock>Propulsion[main][1][1.0]</coupledBlock>
+ </coupledBlocks>
+ <postCouplingBlocks>
+ <postCouplingBlock>Performance[main][1][1.0]</postCouplingBlock>
+ <postCouplingBlock>C[sigmas]</postCouplingBlock>
+ <postCouplingBlock>C[Theta]</postCouplingBlock>
+ <postCouplingBlock>C[dpdx]</postCouplingBlock>
+ <postCouplingBlock>C[prop]</postCouplingBlock>
+ <postCouplingBlock>F[R]</postCouplingBlock>
+ </postCouplingBlocks>
+ </executableBlocks>
+ </problemRoles>
+ </problemDefinition>
+ <workflow>
+ <problemDefinitionUID>converged-DOEGauss-Seidel</problemDefinitionUID>
+ <dataGraph>
+ <name>XDSM - converged-DOE-GS-FF - Mdao</name>
+ <edges>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/dpdx</fromParameterUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WFO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Nz</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/CDmin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WBE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/fin</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma5</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma4</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma3</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma2</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma1</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Nz</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/fin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/SFC</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WFO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/CDmin</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/DT</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WBE</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/Temp</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ </edges>
+ </dataGraph>
+ <processGraph>
+ <name>XDSM - converged-DOE-GS-FF - Mdao</name>
+ <edges>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>9</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>3</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ <processStepNumber>10</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>2</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>1</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>5</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>4</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>6</processStepNumber>
+ </edge>
+ </edges>
+ <nodes>
+ <node>
+ <referenceUID>F[R]</referenceUID>
+ <processStepNumber>8</processStepNumber>
+ <diagonalPosition>11</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Performance[main][1][1.0]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>6</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[Theta]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>8</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[prop]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>10</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Converger</referenceUID>
+ <processStepNumber>2</processStepNumber>
+ <convergerStepNumber>6</convergerStepNumber>
+ <diagonalPosition>2</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>DOE</referenceUID>
+ <processStepNumber>1</processStepNumber>
+ <convergerStepNumber>9</convergerStepNumber>
+ <diagonalPosition>1</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Coordinator</referenceUID>
+ <processStepNumber>0</processStepNumber>
+ <convergerStepNumber>10</convergerStepNumber>
+ <diagonalPosition>0</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[dpdx]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>9</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[sigmas]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>7</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Aerodynamics[main][1][1.0]</referenceUID>
+ <processStepNumber>4</processStepNumber>
+ <diagonalPosition>4</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Structures[main][1][1.0]</referenceUID>
+ <processStepNumber>3</processStepNumber>
+ <diagonalPosition>3</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Propulsion[main][1][1.0]</referenceUID>
+ <processStepNumber>5</processStepNumber>
+ <diagonalPosition>5</diagonalPosition>
+ </node>
+ </nodes>
+ <metadata>
+ <loopNesting>
+ <loopElements>
+ <loopElement relatedUID="Coordinator">
+ <loopElements>
+ <loopElement relatedUID="DOE">
+ <loopElements>
+ <loopElement relatedUID="Converger">
+ <functionElements>
+ <functionElement>Structures[main][1][1.0]</functionElement>
+ <functionElement>Aerodynamics[main][1][1.0]</functionElement>
+ <functionElement>Propulsion[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ <functionElements>
+ <functionElement>C[Theta]</functionElement>
+ <functionElement>F[R]</functionElement>
+ <functionElement>C[dpdx]</functionElement>
+ <functionElement>C[prop]</functionElement>
+ <functionElement>C[sigmas]</functionElement>
+ <functionElement>Performance[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ </loopElement>
+ </loopElements>
+ </loopNesting>
+ </metadata>
+ </processGraph>
+ </workflow>
+ <architectureElements>
+ <parameters>
+ <initialGuessCouplingVariables>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c0}</label>
+ </initialGuessCouplingVariable>
+ </initialGuessCouplingVariables>
+ <finalCouplingVariables>
+ <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{*}</label>
+ </finalCouplingVariable>
+ </finalCouplingVariables>
+ <couplingCopyVariables>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c}</label>
+ </couplingCopyVariable>
+ </couplingCopyVariables>
+ <doeInputSampleLists>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/lambda</relatedParameterUID>
+ <label>DOE_lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h">
+ <relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
+ <label>DOE_h_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
+ <relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
+ <label>DOE_M_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf">
+ <relatedParameterUID>/data_schema/aircraft/other/Cf</relatedParameterUID>
+ <label>DOE_Cf_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Lambda</relatedParameterUID>
+ <label>DOE_Lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T">
+ <relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
+ <label>DOE_T_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc">
+ <relatedParameterUID>/data_schema/aircraft/geometry/tc</relatedParameterUID>
+ <label>DOE_tc_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
+ <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
+ <label>DOE_AR_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
+ <label>DOE_Sref_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section">
+ <relatedParameterUID>/data_schema/aircraft/geometry/section</relatedParameterUID>
+ <label>DOE_section_{inp}</label>
+ </doeInputSampleList>
+ </doeInputSampleLists>
+ <doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</relatedParameterUID>
+ <label>DOE_DT_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</relatedParameterUID>
+ <label>DOE_Temp_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/dpdx</relatedParameterUID>
+ <label>DOE_dpdx_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</relatedParameterUID>
+ <label>DOE_sigma4_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</relatedParameterUID>
+ <label>DOE_sigma3_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</relatedParameterUID>
+ <label>DOE_sigma2_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</relatedParameterUID>
+ <label>DOE_sigma1_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</relatedParameterUID>
+ <label>DOE_sigma5_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/Theta</relatedParameterUID>
+ <label>DOE_Theta_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</relatedParameterUID>
+ <label>DOE_ESF_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R">
+ <relatedParameterUID>/data_schema/mdo_data/objectives/R</relatedParameterUID>
+ <label>DOE_R_{out}</label>
+ </doeOutputSampleList>
+ </doeOutputSampleLists>
+ </parameters>
+ <executableBlocks>
+ <coordinators>
+ <coordinator uID="Coordinator">
+ <label>COOR</label>
+ </coordinator>
+ </coordinators>
+ <convergers>
+ <converger uID="Converger">
+ <label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
+ </converger>
+ </convergers>
+ <does>
+ <doe uID="DOE">
+ <label>DOE</label>
+ <settings>
+ <doeMethod>Full factorial design</doeMethod>
+ <doeRuns>2</doeRuns>
+ </settings>
+ <designVariables>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/Cf</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/AR</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Sref</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/tc</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/M</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/section</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/T</designVariableUID>
+ </designVariable>
+ </designVariables>
+ </doe>
+ </does>
+ <coupledAnalyses>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Structures[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Aerodynamics[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Propulsion[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ </coupledAnalyses>
+ <postCouplingAnalyses>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>F[R]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[prop]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[Theta]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>Performance[main][1][1.0]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[dpdx]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[sigmas]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ </postCouplingAnalyses>
+ </executableBlocks>
+ </architectureElements>
+</cmdows>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml
new file mode 100644
index 0000000000000000000000000000000000000000..42dbfb2c7795e974f50a4a773b11637d0f8b768a
--- /dev/null
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml
@@ -0,0 +1,1855 @@
+<?xml version='1.0' encoding='UTF-8'?>
+<cmdows xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="https://bitbucket.org/imcovangent/cmdows/raw/master/schema/0.7/cmdows.xsd">
+ <header>
+ <creator>Imco van Gent</creator>
+ <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ <updates>
+ <update>
+ <modification>KADMOS export of a mdao data graph (MDG).</modification>
+ <creator>Imco van Gent</creator>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ </update>
+ </updates>
+ </header>
+ <executableBlocks>
+ <designCompetences>
+ <designCompetence uID="Performance[main][1][1.0]">
+ <ID>Performance</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Performance</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Aerodynamics[main][1][1.0]">
+ <ID>Aerodynamics</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Aerodynamics</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/CDmin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/L</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Propulsion[main][1][1.0]">
+ <ID>Propulsion</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Propulsion</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WBE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Structures[main][1][1.0]">
+ <ID>Structures</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Structures</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Nz</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WFO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ </designCompetences>
+ <mathematicalFunctions>
+ <mathematicalFunction uID="F[R]">
+ <label>F[R]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ <equationLabel>R</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ <equations uID="F[R]_equation">
+ <equation language="Python">-R</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[Theta]">
+ <label>C[Theta]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ <equationLabel>Theta</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ <equations uID="C[Theta]_equation">
+ <equation language="Python">Theta/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[dpdx]">
+ <label>C[dpdx]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ <equationLabel>dpdx</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ <equations uID="C[dpdx]_equation">
+ <equation language="Python">dpdx/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[prop]">
+ <label>C[prop]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ <equationLabel>ESF</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ <equationLabel>Temp</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ <equationLabel>DT</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ <equations uID="C[prop]_equation">
+ <equation language="Python">ESF/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ <equations uID="C[prop]_equation_1">
+ <equation language="Python">DT/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ <equations uID="C[prop]_equation_2">
+ <equation language="Python">Temp/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[sigmas]">
+ <label>C[sigmas]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ <equationLabel>sigma5</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ <equationLabel>sigma4</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ <equationLabel>sigma3</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ <equationLabel>sigma2</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ <equationLabel>sigma1</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ <equations uID="C[sigmas]_equation">
+ <equation language="Python">sigma4/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ <equations uID="C[sigmas]_equation_1">
+ <equation language="Python">sigma5/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ <equations uID="C[sigmas]_equation_2">
+ <equation language="Python">sigma1/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ <equations uID="C[sigmas]_equation_3">
+ <equation language="Python">sigma2/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ <equations uID="C[sigmas]_equation_4">
+ <equation language="Python">sigma3/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ </mathematicalFunctions>
+ </executableBlocks>
+ <parameters>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WO">
+ <label>WO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WF">
+ <label>WF</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/L">
+ <label>L</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/D">
+ <label>D</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/fin">
+ <label>fin</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/T">
+ <label>T</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Cf">
+ <label>Cf</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Nz">
+ <label>Nz</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/lambda">
+ <label>lambda</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/objectives/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/SFC">
+ <label>SFC</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WFO">
+ <label>WFO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/CDmin">
+ <label>CDmin</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/section">
+ <label>section</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WBE">
+ <label>WBE</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WT">
+ <label>WT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/AR">
+ <label>AR</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/tc">
+ <label>tc</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Sref">
+ <label>Sref</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/h">
+ <label>h</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/M">
+ <label>M</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Lambda">
+ <label>Lambda</label>
+ </parameter>
+ </parameters>
+ <problemDefinition uID="converged-DOEGauss-Seidel">
+ <problemFormulation>
+ <mdaoArchitecture>converged-DOE</mdaoArchitecture>
+ <convergerType>Gauss-Seidel</convergerType>
+ <executableBlocksOrder>
+ <executableBlock position="1">Structures[main][1][1.0]</executableBlock>
+ <executableBlock position="2">Aerodynamics[main][1][1.0]</executableBlock>
+ <executableBlock position="3">Propulsion[main][1][1.0]</executableBlock>
+ <executableBlock position="4">Performance[main][1][1.0]</executableBlock>
+ <executableBlock position="5">C[sigmas]</executableBlock>
+ <executableBlock position="6">C[Theta]</executableBlock>
+ <executableBlock position="7">C[dpdx]</executableBlock>
+ <executableBlock position="8">C[prop]</executableBlock>
+ <executableBlock position="9">F[R]</executableBlock>
+ </executableBlocksOrder>
+ <allowUnconvergedCouplings>false</allowUnconvergedCouplings>
+ <doeSettings>
+ <doeMethod>Latin hypercube design</doeMethod>
+ <doeRuns>20</doeRuns>
+ </doeSettings>
+ </problemFormulation>
+ <problemRoles>
+ <parameters>
+ <designVariables>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/T">
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ <nominalValue>0.55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>1.0</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.15</sample>
+ <sample position="3">0.2</sample>
+ <sample position="4">0.25</sample>
+ <sample position="5">0.3</sample>
+ <sample position="6">0.35</sample>
+ <sample position="7">0.4</sample>
+ <sample position="8">0.45</sample>
+ <sample position="9">0.5</sample>
+ <sample position="10">0.55</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ <nominalValue>0.25</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>0.4</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.116666666667</sample>
+ <sample position="3">0.133333333333</sample>
+ <sample position="4">0.15</sample>
+ <sample position="5">0.166666666667</sample>
+ <sample position="6">0.183333333333</sample>
+ <sample position="7">0.2</sample>
+ <sample position="8">0.216666666667</sample>
+ <sample position="9">0.233333333333</sample>
+ <sample position="10">0.25</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <nominalValue>5.5</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>2.5</minimum>
+ <maximum>8.5</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">2.5</sample>
+ <sample position="2">2.83333333333</sample>
+ <sample position="3">3.16666666667</sample>
+ <sample position="4">3.5</sample>
+ <sample position="5">3.83333333333</sample>
+ <sample position="6">4.16666666667</sample>
+ <sample position="7">4.5</sample>
+ <sample position="8">4.83333333333</sample>
+ <sample position="9">5.16666666667</sample>
+ <sample position="10">5.5</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <nominalValue>0.05</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.01</minimum>
+ <maximum>0.09</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.01</sample>
+ <sample position="2">0.0144444444444</sample>
+ <sample position="3">0.0188888888889</sample>
+ <sample position="4">0.0233333333333</sample>
+ <sample position="5">0.0277777777778</sample>
+ <sample position="6">0.0322222222222</sample>
+ <sample position="7">0.0366666666667</sample>
+ <sample position="8">0.0411111111111</sample>
+ <sample position="9">0.0455555555556</sample>
+ <sample position="10">0.05</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <nominalValue>1000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>500</minimum>
+ <maximum>1500</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">500.0</sample>
+ <sample position="2">555.555555556</sample>
+ <sample position="3">611.111111111</sample>
+ <sample position="4">666.666666667</sample>
+ <sample position="5">722.222222222</sample>
+ <sample position="6">777.777777778</sample>
+ <sample position="7">833.333333333</sample>
+ <sample position="8">888.888888889</sample>
+ <sample position="9">944.444444444</sample>
+ <sample position="10">1000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/h">
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <nominalValue>45000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>30000</minimum>
+ <maximum>60000</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">30000.0</sample>
+ <sample position="2">31666.6666667</sample>
+ <sample position="3">33333.3333333</sample>
+ <sample position="4">35000.0</sample>
+ <sample position="5">36666.6666667</sample>
+ <sample position="6">38333.3333333</sample>
+ <sample position="7">40000.0</sample>
+ <sample position="8">41666.6666667</sample>
+ <sample position="9">43333.3333333</sample>
+ <sample position="10">45000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/M">
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <nominalValue>1.6</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>1.4</minimum>
+ <maximum>1.8</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">1.4</sample>
+ <sample position="2">1.42222222222</sample>
+ <sample position="3">1.44444444444</sample>
+ <sample position="4">1.46666666667</sample>
+ <sample position="5">1.48888888889</sample>
+ <sample position="6">1.51111111111</sample>
+ <sample position="7">1.53333333333</sample>
+ <sample position="8">1.55555555556</sample>
+ <sample position="9">1.57777777778</sample>
+ <sample position="10">1.6</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <nominalValue>55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>40</minimum>
+ <maximum>70</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">40.0</sample>
+ <sample position="2">41.6666666667</sample>
+ <sample position="3">43.3333333333</sample>
+ <sample position="4">45.0</sample>
+ <sample position="5">46.6666666667</sample>
+ <sample position="6">48.3333333333</sample>
+ <sample position="7">50.0</sample>
+ <sample position="8">51.6666666667</sample>
+ <sample position="9">53.3333333333</sample>
+ <sample position="10">55.0</sample>
+ </samples>
+ </designVariable>
+ </designVariables>
+ <stateVariables>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/DT">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/Theta">
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/Temp">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/dpdx">
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
+ </stateVariables>
+ </parameters>
+ <executableBlocks>
+ <coupledBlocks>
+ <coupledBlock>Structures[main][1][1.0]</coupledBlock>
+ <coupledBlock>Aerodynamics[main][1][1.0]</coupledBlock>
+ <coupledBlock>Propulsion[main][1][1.0]</coupledBlock>
+ </coupledBlocks>
+ <postCouplingBlocks>
+ <postCouplingBlock>Performance[main][1][1.0]</postCouplingBlock>
+ <postCouplingBlock>C[sigmas]</postCouplingBlock>
+ <postCouplingBlock>C[Theta]</postCouplingBlock>
+ <postCouplingBlock>C[dpdx]</postCouplingBlock>
+ <postCouplingBlock>C[prop]</postCouplingBlock>
+ <postCouplingBlock>F[R]</postCouplingBlock>
+ </postCouplingBlocks>
+ </executableBlocks>
+ </problemRoles>
+ </problemDefinition>
+ <workflow>
+ <problemDefinitionUID>converged-DOEGauss-Seidel</problemDefinitionUID>
+ <dataGraph>
+ <name>XDSM - converged-DOE-GS-LH - Mdao</name>
+ <edges>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/dpdx</fromParameterUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WFO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Nz</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/CDmin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WBE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/fin</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma5</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma4</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma3</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma2</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma1</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Nz</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/fin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/SFC</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WFO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/CDmin</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/DT</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WBE</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/Temp</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ </edges>
+ </dataGraph>
+ <processGraph>
+ <name>XDSM - converged-DOE-GS-LH - Mdao</name>
+ <edges>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>9</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>3</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ <processStepNumber>10</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>2</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>1</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>5</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>4</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>6</processStepNumber>
+ </edge>
+ </edges>
+ <nodes>
+ <node>
+ <referenceUID>F[R]</referenceUID>
+ <processStepNumber>8</processStepNumber>
+ <diagonalPosition>11</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Performance[main][1][1.0]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>6</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[Theta]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>8</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[prop]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>10</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Converger</referenceUID>
+ <processStepNumber>2</processStepNumber>
+ <convergerStepNumber>6</convergerStepNumber>
+ <diagonalPosition>2</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>DOE</referenceUID>
+ <processStepNumber>1</processStepNumber>
+ <convergerStepNumber>9</convergerStepNumber>
+ <diagonalPosition>1</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Coordinator</referenceUID>
+ <processStepNumber>0</processStepNumber>
+ <convergerStepNumber>10</convergerStepNumber>
+ <diagonalPosition>0</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[dpdx]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>9</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[sigmas]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>7</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Aerodynamics[main][1][1.0]</referenceUID>
+ <processStepNumber>4</processStepNumber>
+ <diagonalPosition>4</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Structures[main][1][1.0]</referenceUID>
+ <processStepNumber>3</processStepNumber>
+ <diagonalPosition>3</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Propulsion[main][1][1.0]</referenceUID>
+ <processStepNumber>5</processStepNumber>
+ <diagonalPosition>5</diagonalPosition>
+ </node>
+ </nodes>
+ <metadata>
+ <loopNesting>
+ <loopElements>
+ <loopElement relatedUID="Coordinator">
+ <loopElements>
+ <loopElement relatedUID="DOE">
+ <loopElements>
+ <loopElement relatedUID="Converger">
+ <functionElements>
+ <functionElement>Structures[main][1][1.0]</functionElement>
+ <functionElement>Aerodynamics[main][1][1.0]</functionElement>
+ <functionElement>Propulsion[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ <functionElements>
+ <functionElement>C[Theta]</functionElement>
+ <functionElement>F[R]</functionElement>
+ <functionElement>C[dpdx]</functionElement>
+ <functionElement>C[prop]</functionElement>
+ <functionElement>C[sigmas]</functionElement>
+ <functionElement>Performance[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ </loopElement>
+ </loopElements>
+ </loopNesting>
+ </metadata>
+ </processGraph>
+ </workflow>
+ <architectureElements>
+ <parameters>
+ <initialGuessCouplingVariables>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c0}</label>
+ </initialGuessCouplingVariable>
+ </initialGuessCouplingVariables>
+ <finalCouplingVariables>
+ <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{*}</label>
+ </finalCouplingVariable>
+ </finalCouplingVariables>
+ <couplingCopyVariables>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c}</label>
+ </couplingCopyVariable>
+ </couplingCopyVariables>
+ <doeInputSampleLists>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/lambda</relatedParameterUID>
+ <label>DOE_lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h">
+ <relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
+ <label>DOE_h_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
+ <relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
+ <label>DOE_M_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf">
+ <relatedParameterUID>/data_schema/aircraft/other/Cf</relatedParameterUID>
+ <label>DOE_Cf_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Lambda</relatedParameterUID>
+ <label>DOE_Lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T">
+ <relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
+ <label>DOE_T_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc">
+ <relatedParameterUID>/data_schema/aircraft/geometry/tc</relatedParameterUID>
+ <label>DOE_tc_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
+ <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
+ <label>DOE_AR_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
+ <label>DOE_Sref_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section">
+ <relatedParameterUID>/data_schema/aircraft/geometry/section</relatedParameterUID>
+ <label>DOE_section_{inp}</label>
+ </doeInputSampleList>
+ </doeInputSampleLists>
+ <doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</relatedParameterUID>
+ <label>DOE_DT_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</relatedParameterUID>
+ <label>DOE_Temp_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/dpdx</relatedParameterUID>
+ <label>DOE_dpdx_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</relatedParameterUID>
+ <label>DOE_sigma4_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</relatedParameterUID>
+ <label>DOE_sigma3_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</relatedParameterUID>
+ <label>DOE_sigma2_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</relatedParameterUID>
+ <label>DOE_sigma1_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</relatedParameterUID>
+ <label>DOE_sigma5_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/Theta</relatedParameterUID>
+ <label>DOE_Theta_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</relatedParameterUID>
+ <label>DOE_ESF_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R">
+ <relatedParameterUID>/data_schema/mdo_data/objectives/R</relatedParameterUID>
+ <label>DOE_R_{out}</label>
+ </doeOutputSampleList>
+ </doeOutputSampleLists>
+ </parameters>
+ <executableBlocks>
+ <coordinators>
+ <coordinator uID="Coordinator">
+ <label>COOR</label>
+ </coordinator>
+ </coordinators>
+ <convergers>
+ <converger uID="Converger">
+ <label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
+ </converger>
+ </convergers>
+ <does>
+ <doe uID="DOE">
+ <label>DOE</label>
+ <settings>
+ <doeMethod>Latin hypercube design</doeMethod>
+ <doeRuns>20</doeRuns>
+ <doeSeed>5</doeSeed>
+ </settings>
+ <designVariables>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/Cf</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/AR</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Sref</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/tc</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/M</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/section</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/T</designVariableUID>
+ </designVariable>
+ </designVariables>
+ </doe>
+ </does>
+ <coupledAnalyses>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Structures[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Aerodynamics[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Propulsion[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ </coupledAnalyses>
+ <postCouplingAnalyses>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>F[R]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[prop]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[Theta]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>Performance[main][1][1.0]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[dpdx]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[sigmas]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ </postCouplingAnalyses>
+ </executableBlocks>
+ </architectureElements>
+</cmdows>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml
new file mode 100644
index 0000000000000000000000000000000000000000..3df994ef927e63b197afae010c2de4789f9e8451
--- /dev/null
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml
@@ -0,0 +1,1855 @@
+<?xml version='1.0' encoding='UTF-8'?>
+<cmdows xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="https://bitbucket.org/imcovangent/cmdows/raw/master/schema/0.7/cmdows.xsd">
+ <header>
+ <creator>Imco van Gent</creator>
+ <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ <updates>
+ <update>
+ <modification>KADMOS export of a mdao data graph (MDG).</modification>
+ <creator>Imco van Gent</creator>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
+ <fileVersion>0.1</fileVersion>
+ <cmdowsVersion>0.7</cmdowsVersion>
+ </update>
+ </updates>
+ </header>
+ <executableBlocks>
+ <designCompetences>
+ <designCompetence uID="Performance[main][1][1.0]">
+ <ID>Performance</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Performance</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Aerodynamics[main][1][1.0]">
+ <ID>Aerodynamics</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Aerodynamics</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/CDmin</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/fin</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/L</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Propulsion[main][1][1.0]">
+ <ID>Propulsion</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Propulsion</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WBE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/D</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ <designCompetence uID="Structures[main][1][1.0]">
+ <ID>Structures</ID>
+ <modeID>main</modeID>
+ <instanceID>1</instanceID>
+ <version>1.0</version>
+ <label>Structures</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/Nz</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WFO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/weight/WO</parameterUID>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ </output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
+ </output>
+ </outputs>
+ </designCompetence>
+ </designCompetences>
+ <mathematicalFunctions>
+ <mathematicalFunction uID="F[R]">
+ <label>F[R]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/R</parameterUID>
+ <equationLabel>R</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ <equations uID="F[R]_equation">
+ <equation language="Python">-R</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[Theta]">
+ <label>C[Theta]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
+ <equationLabel>Theta</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ <equations uID="C[Theta]_equation">
+ <equation language="Python">Theta/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[dpdx]">
+ <label>C[dpdx]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
+ <equationLabel>dpdx</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ <equations uID="C[dpdx]_equation">
+ <equation language="Python">dpdx/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[prop]">
+ <label>C[prop]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/reference/ESF</parameterUID>
+ <equationLabel>ESF</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/reference/Temp</parameterUID>
+ <equationLabel>Temp</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/DT</parameterUID>
+ <equationLabel>DT</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ <equations uID="C[prop]_equation">
+ <equation language="Python">ESF/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ <equations uID="C[prop]_equation_1">
+ <equation language="Python">DT/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ <equations uID="C[prop]_equation_2">
+ <equation language="Python">Temp/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ <mathematicalFunction uID="C[sigmas]">
+ <label>C[sigmas]</label>
+ <inputs>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma5</parameterUID>
+ <equationLabel>sigma5</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma4</parameterUID>
+ <equationLabel>sigma4</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma3</parameterUID>
+ <equationLabel>sigma3</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma2</parameterUID>
+ <equationLabel>sigma2</equationLabel>
+ </input>
+ <input>
+ <parameterUID>/data_schema/aircraft/other/sigma1</parameterUID>
+ <equationLabel>sigma1</equationLabel>
+ </input>
+ </inputs>
+ <outputs>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ <equations uID="C[sigmas]_equation">
+ <equation language="Python">sigma4/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ <equations uID="C[sigmas]_equation_1">
+ <equation language="Python">sigma5/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ <equations uID="C[sigmas]_equation_2">
+ <equation language="Python">sigma1/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ <equations uID="C[sigmas]_equation_3">
+ <equation language="Python">sigma2/1.0</equation>
+ </equations>
+ </output>
+ <output>
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ <equations uID="C[sigmas]_equation_4">
+ <equation language="Python">sigma3/1.0</equation>
+ </equations>
+ </output>
+ </outputs>
+ </mathematicalFunction>
+ </mathematicalFunctions>
+ </executableBlocks>
+ <parameters>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WO">
+ <label>WO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WF">
+ <label>WF</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/L">
+ <label>L</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/D">
+ <label>D</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/fin">
+ <label>fin</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/T">
+ <label>T</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma3">
+ <label>sigma3</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Cf">
+ <label>Cf</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/Nz">
+ <label>Nz</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/lambda">
+ <label>lambda</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/objectives/R">
+ <label>R</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/SFC">
+ <label>SFC</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WFO">
+ <label>WFO</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/CDmin">
+ <label>CDmin</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/section">
+ <label>section</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/other/DT">
+ <label>DT</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/propulsion/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <label>sigma4</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <label>sigma5</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <label>sigma1</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <label>sigma2</label>
+ </parameter>
+ <parameter uID="/data_schema/mdo_data/constraints/dpdx">
+ <label>dpdx</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WBE">
+ <label>WBE</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/Temp">
+ <label>Temp</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Theta">
+ <label>Theta</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WT">
+ <label>WT</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/AR">
+ <label>AR</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/tc">
+ <label>tc</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/ESF">
+ <label>ESF</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Sref">
+ <label>Sref</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/h">
+ <label>h</label>
+ </parameter>
+ <parameter uID="/data_schema/reference/M">
+ <label>M</label>
+ </parameter>
+ <parameter uID="/data_schema/aircraft/geometry/Lambda">
+ <label>Lambda</label>
+ </parameter>
+ </parameters>
+ <problemDefinition uID="converged-DOEGauss-Seidel">
+ <problemFormulation>
+ <mdaoArchitecture>converged-DOE</mdaoArchitecture>
+ <convergerType>Gauss-Seidel</convergerType>
+ <executableBlocksOrder>
+ <executableBlock position="1">Structures[main][1][1.0]</executableBlock>
+ <executableBlock position="2">Aerodynamics[main][1][1.0]</executableBlock>
+ <executableBlock position="3">Propulsion[main][1][1.0]</executableBlock>
+ <executableBlock position="4">Performance[main][1][1.0]</executableBlock>
+ <executableBlock position="5">C[sigmas]</executableBlock>
+ <executableBlock position="6">C[Theta]</executableBlock>
+ <executableBlock position="7">C[dpdx]</executableBlock>
+ <executableBlock position="8">C[prop]</executableBlock>
+ <executableBlock position="9">F[R]</executableBlock>
+ </executableBlocksOrder>
+ <allowUnconvergedCouplings>false</allowUnconvergedCouplings>
+ <doeSettings>
+ <doeMethod>Monte Carlo design</doeMethod>
+ <doeRuns>10</doeRuns>
+ </doeSettings>
+ </problemFormulation>
+ <problemRoles>
+ <parameters>
+ <designVariables>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/T">
+ <parameterUID>/data_schema/aircraft/other/T</parameterUID>
+ <nominalValue>0.55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>1.0</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.15</sample>
+ <sample position="3">0.2</sample>
+ <sample position="4">0.25</sample>
+ <sample position="5">0.3</sample>
+ <sample position="6">0.35</sample>
+ <sample position="7">0.4</sample>
+ <sample position="8">0.45</sample>
+ <sample position="9">0.5</sample>
+ <sample position="10">0.55</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
+ <parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
+ <parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
+ <nominalValue>0.25</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.1</minimum>
+ <maximum>0.4</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.1</sample>
+ <sample position="2">0.116666666667</sample>
+ <sample position="3">0.133333333333</sample>
+ <sample position="4">0.15</sample>
+ <sample position="5">0.166666666667</sample>
+ <sample position="6">0.183333333333</sample>
+ <sample position="7">0.2</sample>
+ <sample position="8">0.216666666667</sample>
+ <sample position="9">0.233333333333</sample>
+ <sample position="10">0.25</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
+ <parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
+ <nominalValue>1.0</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.75</minimum>
+ <maximum>1.25</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.75</sample>
+ <sample position="2">0.777777777778</sample>
+ <sample position="3">0.805555555556</sample>
+ <sample position="4">0.833333333333</sample>
+ <sample position="5">0.861111111111</sample>
+ <sample position="6">0.888888888889</sample>
+ <sample position="7">0.916666666667</sample>
+ <sample position="8">0.944444444444</sample>
+ <sample position="9">0.972222222222</sample>
+ <sample position="10">1.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
+ <parameterUID>/data_schema/aircraft/geometry/AR</parameterUID>
+ <nominalValue>5.5</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>2.5</minimum>
+ <maximum>8.5</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">2.5</sample>
+ <sample position="2">2.83333333333</sample>
+ <sample position="3">3.16666666667</sample>
+ <sample position="4">3.5</sample>
+ <sample position="5">3.83333333333</sample>
+ <sample position="6">4.16666666667</sample>
+ <sample position="7">4.5</sample>
+ <sample position="8">4.83333333333</sample>
+ <sample position="9">5.16666666667</sample>
+ <sample position="10">5.5</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
+ <parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
+ <nominalValue>0.05</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>0.01</minimum>
+ <maximum>0.09</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">0.01</sample>
+ <sample position="2">0.0144444444444</sample>
+ <sample position="3">0.0188888888889</sample>
+ <sample position="4">0.0233333333333</sample>
+ <sample position="5">0.0277777777778</sample>
+ <sample position="6">0.0322222222222</sample>
+ <sample position="7">0.0366666666667</sample>
+ <sample position="8">0.0411111111111</sample>
+ <sample position="9">0.0455555555556</sample>
+ <sample position="10">0.05</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
+ <parameterUID>/data_schema/aircraft/geometry/Sref</parameterUID>
+ <nominalValue>1000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>500</minimum>
+ <maximum>1500</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">500.0</sample>
+ <sample position="2">555.555555556</sample>
+ <sample position="3">611.111111111</sample>
+ <sample position="4">666.666666667</sample>
+ <sample position="5">722.222222222</sample>
+ <sample position="6">777.777777778</sample>
+ <sample position="7">833.333333333</sample>
+ <sample position="8">888.888888889</sample>
+ <sample position="9">944.444444444</sample>
+ <sample position="10">1000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/h">
+ <parameterUID>/data_schema/reference/h</parameterUID>
+ <nominalValue>45000</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>30000</minimum>
+ <maximum>60000</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">30000.0</sample>
+ <sample position="2">31666.6666667</sample>
+ <sample position="3">33333.3333333</sample>
+ <sample position="4">35000.0</sample>
+ <sample position="5">36666.6666667</sample>
+ <sample position="6">38333.3333333</sample>
+ <sample position="7">40000.0</sample>
+ <sample position="8">41666.6666667</sample>
+ <sample position="9">43333.3333333</sample>
+ <sample position="10">45000.0</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/reference/M">
+ <parameterUID>/data_schema/reference/M</parameterUID>
+ <nominalValue>1.6</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>1.4</minimum>
+ <maximum>1.8</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">1.4</sample>
+ <sample position="2">1.42222222222</sample>
+ <sample position="3">1.44444444444</sample>
+ <sample position="4">1.46666666667</sample>
+ <sample position="5">1.48888888889</sample>
+ <sample position="6">1.51111111111</sample>
+ <sample position="7">1.53333333333</sample>
+ <sample position="8">1.55555555556</sample>
+ <sample position="9">1.57777777778</sample>
+ <sample position="10">1.6</sample>
+ </samples>
+ </designVariable>
+ <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
+ <parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
+ <nominalValue>55</nominalValue>
+ <validRanges>
+ <limitRange>
+ <minimum>40</minimum>
+ <maximum>70</maximum>
+ </limitRange>
+ </validRanges>
+ <samples>
+ <sample position="1">40.0</sample>
+ <sample position="2">41.6666666667</sample>
+ <sample position="3">43.3333333333</sample>
+ <sample position="4">45.0</sample>
+ <sample position="5">46.6666666667</sample>
+ <sample position="6">48.3333333333</sample>
+ <sample position="7">50.0</sample>
+ <sample position="8">51.6666666667</sample>
+ <sample position="9">53.3333333333</sample>
+ <sample position="10">55.0</sample>
+ </samples>
+ </designVariable>
+ </designVariables>
+ <stateVariables>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma3">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/DT">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/Theta">
+ <parameterUID>/data_schema/mdo_data/constraints/Theta</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
+ <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/Temp">
+ <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma4">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma1">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma2">
+ <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/dpdx">
+ <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+ </stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
+ </stateVariables>
+ </parameters>
+ <executableBlocks>
+ <coupledBlocks>
+ <coupledBlock>Structures[main][1][1.0]</coupledBlock>
+ <coupledBlock>Aerodynamics[main][1][1.0]</coupledBlock>
+ <coupledBlock>Propulsion[main][1][1.0]</coupledBlock>
+ </coupledBlocks>
+ <postCouplingBlocks>
+ <postCouplingBlock>Performance[main][1][1.0]</postCouplingBlock>
+ <postCouplingBlock>C[sigmas]</postCouplingBlock>
+ <postCouplingBlock>C[Theta]</postCouplingBlock>
+ <postCouplingBlock>C[dpdx]</postCouplingBlock>
+ <postCouplingBlock>C[prop]</postCouplingBlock>
+ <postCouplingBlock>F[R]</postCouplingBlock>
+ </postCouplingBlocks>
+ </executableBlocks>
+ </problemRoles>
+ </problemDefinition>
+ <workflow>
+ <problemDefinitionUID>converged-DOEGauss-Seidel</problemDefinitionUID>
+ <dataGraph>
+ <name>XDSM - converged-DOE-GS-MC - Mdao</name>
+ <edges>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/dpdx</fromParameterUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WFO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Nz</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WO</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/CDmin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WBE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/fin</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma5</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma4</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma3</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma2</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/sigma1</fromParameterUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Cf</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/Nz</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/T</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/fin</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/Theta</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/dpdx</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/SFC</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WFO</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/reference/Temp</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/CDmin</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/other/DT</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/mdo_data/constraints/dpdx</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/h</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WBE</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/M</fromParameterUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ </edge>
+ <edge>
+ <fromParameterUID>/data_schema/reference/Temp</fromParameterUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ </edge>
+ </edges>
+ </dataGraph>
+ <processGraph>
+ <name>XDSM - converged-DOE-GS-MC - Mdao</name>
+ <edges>
+ <edge>
+ <fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>9</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[Theta]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[prop]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[Theta]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[prop]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>3</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[dpdx]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Converger</fromExecutableBlockUID>
+ <toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
+ <processStepNumber>7</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ <processStepNumber>10</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>2</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ <processStepNumber>1</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[dpdx]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
+ <toExecutableBlockUID>F[R]</toExecutableBlockUID>
+ <processStepNumber>8</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>5</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Structures[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
+ <processStepNumber>4</processStepNumber>
+ </edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toExecutableBlockUID>Converger</toExecutableBlockUID>
+ <processStepNumber>6</processStepNumber>
+ </edge>
+ </edges>
+ <nodes>
+ <node>
+ <referenceUID>F[R]</referenceUID>
+ <processStepNumber>8</processStepNumber>
+ <diagonalPosition>11</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Performance[main][1][1.0]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>6</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[Theta]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>8</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[prop]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>10</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Converger</referenceUID>
+ <processStepNumber>2</processStepNumber>
+ <convergerStepNumber>6</convergerStepNumber>
+ <diagonalPosition>2</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>DOE</referenceUID>
+ <processStepNumber>1</processStepNumber>
+ <convergerStepNumber>9</convergerStepNumber>
+ <diagonalPosition>1</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Coordinator</referenceUID>
+ <processStepNumber>0</processStepNumber>
+ <convergerStepNumber>10</convergerStepNumber>
+ <diagonalPosition>0</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[dpdx]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>9</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>C[sigmas]</referenceUID>
+ <processStepNumber>7</processStepNumber>
+ <diagonalPosition>7</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Aerodynamics[main][1][1.0]</referenceUID>
+ <processStepNumber>4</processStepNumber>
+ <diagonalPosition>4</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Structures[main][1][1.0]</referenceUID>
+ <processStepNumber>3</processStepNumber>
+ <diagonalPosition>3</diagonalPosition>
+ </node>
+ <node>
+ <referenceUID>Propulsion[main][1][1.0]</referenceUID>
+ <processStepNumber>5</processStepNumber>
+ <diagonalPosition>5</diagonalPosition>
+ </node>
+ </nodes>
+ <metadata>
+ <loopNesting>
+ <loopElements>
+ <loopElement relatedUID="Coordinator">
+ <loopElements>
+ <loopElement relatedUID="DOE">
+ <loopElements>
+ <loopElement relatedUID="Converger">
+ <functionElements>
+ <functionElement>Structures[main][1][1.0]</functionElement>
+ <functionElement>Aerodynamics[main][1][1.0]</functionElement>
+ <functionElement>Propulsion[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ <functionElements>
+ <functionElement>C[Theta]</functionElement>
+ <functionElement>F[R]</functionElement>
+ <functionElement>C[dpdx]</functionElement>
+ <functionElement>C[prop]</functionElement>
+ <functionElement>C[sigmas]</functionElement>
+ <functionElement>Performance[main][1][1.0]</functionElement>
+ </functionElements>
+ </loopElement>
+ </loopElements>
+ </loopElement>
+ </loopElements>
+ </loopNesting>
+ </metadata>
+ </processGraph>
+ </workflow>
+ <architectureElements>
+ <parameters>
+ <initialGuessCouplingVariables>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c0}</label>
+ </initialGuessCouplingVariable>
+ <initialGuessCouplingVariable uID="/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c0}</label>
+ </initialGuessCouplingVariable>
+ </initialGuessCouplingVariables>
+ <finalCouplingVariables>
+ <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{*}</label>
+ </finalCouplingVariable>
+ </finalCouplingVariables>
+ <couplingCopyVariables>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L">
+ <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+ <label>L^{c}</label>
+ </couplingCopyVariable>
+ <couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF">
+ <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
+ <label>ESF^{c}</label>
+ </couplingCopyVariable>
+ </couplingCopyVariables>
+ <doeInputSampleLists>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/lambda</relatedParameterUID>
+ <label>DOE_lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/h">
+ <relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
+ <label>DOE_h_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
+ <relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
+ <label>DOE_M_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/Cf">
+ <relatedParameterUID>/data_schema/aircraft/other/Cf</relatedParameterUID>
+ <label>DOE_Cf_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Lambda">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Lambda</relatedParameterUID>
+ <label>DOE_Lambda_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T">
+ <relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
+ <label>DOE_T_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc">
+ <relatedParameterUID>/data_schema/aircraft/geometry/tc</relatedParameterUID>
+ <label>DOE_tc_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
+ <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
+ <label>DOE_AR_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
+ <label>DOE_Sref_{inp}</label>
+ </doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/section">
+ <relatedParameterUID>/data_schema/aircraft/geometry/section</relatedParameterUID>
+ <label>DOE_section_{inp}</label>
+ </doeInputSampleList>
+ </doeInputSampleLists>
+ <doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/DT</relatedParameterUID>
+ <label>DOE_DT_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</relatedParameterUID>
+ <label>DOE_Temp_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/dpdx</relatedParameterUID>
+ <label>DOE_dpdx_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</relatedParameterUID>
+ <label>DOE_sigma4_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma3</relatedParameterUID>
+ <label>DOE_sigma3_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma2</relatedParameterUID>
+ <label>DOE_sigma2_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma1</relatedParameterUID>
+ <label>DOE_sigma1_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</relatedParameterUID>
+ <label>DOE_sigma5_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/Theta</relatedParameterUID>
+ <label>DOE_Theta_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/ESF">
+ <relatedParameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</relatedParameterUID>
+ <label>DOE_ESF_{out}</label>
+ </doeOutputSampleList>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R">
+ <relatedParameterUID>/data_schema/mdo_data/objectives/R</relatedParameterUID>
+ <label>DOE_R_{out}</label>
+ </doeOutputSampleList>
+ </doeOutputSampleLists>
+ </parameters>
+ <executableBlocks>
+ <coordinators>
+ <coordinator uID="Coordinator">
+ <label>COOR</label>
+ </coordinator>
+ </coordinators>
+ <convergers>
+ <converger uID="Converger">
+ <label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
+ </converger>
+ </convergers>
+ <does>
+ <doe uID="DOE">
+ <label>DOE</label>
+ <settings>
+ <doeMethod>Monte Carlo design</doeMethod>
+ <doeRuns>10</doeRuns>
+ <doeSeed>9</doeSeed>
+ </settings>
+ <designVariables>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/h</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/Cf</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/AR</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Sref</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/tc</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/reference/M</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/Lambda</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/geometry/section</designVariableUID>
+ </designVariable>
+ <designVariable>
+ <designVariableUID>__desVar__/data_schema/aircraft/other/T</designVariableUID>
+ </designVariable>
+ </designVariables>
+ </doe>
+ </does>
+ <coupledAnalyses>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Structures[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Aerodynamics[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ <coupledAnalysis>
+ <relatedExecutableBlockUID>Propulsion[main][1][1.0]</relatedExecutableBlockUID>
+ </coupledAnalysis>
+ </coupledAnalyses>
+ <postCouplingAnalyses>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>F[R]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[prop]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[Theta]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>Performance[main][1][1.0]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[dpdx]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ <postCouplingAnalysis>
+ <relatedExecutableBlockUID>C[sigmas]</relatedExecutableBlockUID>
+ </postCouplingAnalysis>
+ </postCouplingAnalyses>
+ </executableBlocks>
+ </architectureElements>
+</cmdows>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
similarity index 97%
rename from examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J.xml
rename to examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
index 324ad4081dbfe3148304a46d18af3d88293d4c65..2e35af847ceea7c96084ff95f4cd371b4db92555 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -130,9 +130,15 @@
</input>
</inputs>
<outputs>
+ <output>
+ <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/reference/ESF</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/reference/Temp</parameterUID>
</output>
@@ -142,9 +148,6 @@
<output>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
</output>
- <output>
- <parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
- </output>
</outputs>
</designCompetence>
<designCompetence uID="Structures[main][1][1.0]">
@@ -222,14 +225,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -374,9 +377,6 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
- <parameter uID="/data_schema/aircraft/weight/WE">
- <label>WE</label>
- </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -476,6 +476,9 @@
<parameter uID="/data_schema/aircraft/weight/WT">
<label>WT</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/geometry/AR">
<label>AR</label>
</parameter>
@@ -776,6 +779,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
<parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
</stateVariables>
</parameters>
<executableBlocks>
@@ -798,7 +804,7 @@
<workflow>
<problemDefinitionUID>converged-DOEJacobi</problemDefinitionUID>
<dataGraph>
- <name>XDSM - converged-DOE-J - Mdao</name>
+ <name>XDSM - converged-DOE-J-CT - Mdao</name>
<edges>
<edge>
<fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/lambda</fromParameterUID>
@@ -820,6 +826,10 @@
<fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta</fromParameterUID>
<toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
@@ -888,6 +898,10 @@
<fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>Converger</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
@@ -912,6 +926,10 @@
<fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
<toExecutableBlockUID>Converger</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Coordinator</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M</toParameterUID>
@@ -1110,51 +1128,51 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/h</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
@@ -1166,24 +1184,28 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/M</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
@@ -1272,25 +1294,29 @@
<fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
<toExecutableBlockUID>Coordinator</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/ESF</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
+ <toParameterUID>/data_schema/reference/Temp</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>Converger</fromExecutableBlockUID>
@@ -1463,7 +1489,7 @@
</edges>
</dataGraph>
<processGraph>
- <name>XDSM - converged-DOE-J - Mdao</name>
+ <name>XDSM - converged-DOE-J-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -1690,6 +1716,12 @@
<label>Theta^{c0}</label>
</initialGuessCouplingVariable>
</initialGuessCouplingVariables>
+ <finalCouplingVariables>
+ <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>WE^{*}</label>
+ </finalCouplingVariable>
+ </finalCouplingVariables>
<couplingCopyVariables>
<couplingCopyVariable uID="/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta">
<relatedParameterUID>/data_schema/aircraft/geometry/Theta</relatedParameterUID>
@@ -1759,6 +1791,10 @@
</doeInputSampleList>
</doeInputSampleLists>
<doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
<doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta">
<relatedParameterUID>/data_schema/mdo_data/constraints/Theta</relatedParameterUID>
<label>DOE_Theta_{out}</label>
@@ -1814,12 +1850,19 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<does>
<doe uID="DOE">
<label>DOE</label>
<settings>
+ <doeMethod>Custom design table</doeMethod>
<doeTable>
<tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
<tableElement experimentID="0">0.1</tableElement>
@@ -1942,7 +1985,6 @@
<tableElement experimentID="9">1.6</tableElement>
</tableRow>
</doeTable>
- <doeMethod>Custom design table</doeMethod>
</settings>
<designVariables>
<designVariable>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
index bfa0f278bef0bb479f4e90c8535f7e1230eaea31..a57206d74af46798c3b2163300ac14883f75b865 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -231,14 +231,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -551,6 +551,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -1278,6 +1281,12 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<coupledAnalyses>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
index a46c9664362cacf61b6d915e34150135b5c6b65e..2d3c77243191d4def13dfbf72f88d38350a5a576 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -240,14 +240,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -560,6 +560,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -1405,6 +1408,12 @@
<convergers>
<converger uID="Converger">
<label>CONV</label>
+ <settings>
+ <lastIterationsToConsider>1</lastIterationsToConsider>
+ <maximumIterations>100</maximumIterations>
+ <convergenceToleranceRelative>1e-06</convergenceToleranceRelative>
+ <convergenceToleranceAbsolute>1e-06</convergenceToleranceAbsolute>
+ </settings>
</converger>
</convergers>
<coupledAnalyses>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
similarity index 97%
rename from examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS.xml
rename to examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
index e4ef4c85282469147bfa8ffc13560feb60b3a8f2..3fbd54ae7b224b45f8ce6337aaa8daa7b20fe0bf 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -51,6 +51,9 @@
<output>
<parameterUID>/data_schema/aircraft/other/DT</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
</output>
@@ -216,14 +219,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -425,6 +428,9 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -758,6 +764,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
<parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -786,7 +795,7 @@
<workflow>
<problemDefinitionUID>unconverged-DOEGauss-Seidel</problemDefinitionUID>
<dataGraph>
- <name>XDSM - unconverged-DOE-GS - Mdao</name>
+ <name>XDSM - unconverged-DOE-GS-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -800,6 +809,10 @@
<fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
<toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
<edge>
<fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
<toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</toParameterUID>
@@ -832,6 +845,10 @@
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
@@ -854,51 +871,51 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/h</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
@@ -910,24 +927,28 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/M</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
@@ -988,6 +1009,10 @@
<fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</fromParameterUID>
<toExecutableBlockUID>DOE</toExecutableBlockUID>
@@ -1173,7 +1198,7 @@
<toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
</edge>
<edge>
- <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>DOE</toExecutableBlockUID>
</edge>
<edge>
@@ -1359,7 +1384,7 @@
</edges>
</dataGraph>
<processGraph>
- <name>XDSM - unconverged-DOE-GS - Mdao</name>
+ <name>XDSM - unconverged-DOE-GS-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -1547,6 +1572,10 @@
<relatedParameterUID>/data_schema/aircraft/geometry/lambda</relatedParameterUID>
<label>DOE_lambda_{inp}</label>
</doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
+ <label>DOE_Sref_{inp}</label>
+ </doeInputSampleList>
<doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc">
<relatedParameterUID>/data_schema/aircraft/geometry/tc</relatedParameterUID>
<label>DOE_tc_{inp}</label>
@@ -1559,10 +1588,6 @@
<relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
<label>DOE_h_{inp}</label>
</doeInputSampleList>
- <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
- <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
- <label>DOE_Sref_{inp}</label>
- </doeInputSampleList>
<doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
<relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
<label>DOE_M_{inp}</label>
@@ -1585,6 +1610,10 @@
</doeInputSampleList>
</doeInputSampleLists>
<doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
<doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4">
<relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</relatedParameterUID>
<label>DOE_sigma4_{out}</label>
@@ -1641,6 +1670,7 @@
<doe uID="DOE">
<label>DOE</label>
<settings>
+ <doeMethod>Custom design table</doeMethod>
<doeTable>
<tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
<tableElement experimentID="0">0.1</tableElement>
@@ -1763,7 +1793,6 @@
<tableElement experimentID="9">1.6</tableElement>
</tableRow>
</doeTable>
- <doeMethod>Custom design table</doeMethod>
</settings>
<designVariables>
<designVariable>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
similarity index 98%
rename from examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J.xml
rename to examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
index 9091eac1c076e996c63cdf7d1de8fdcf266c7343..b0bb7f4b0d5a562fb1742d292d00efaa4b0ca3ef 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -51,6 +51,9 @@
<output>
<parameterUID>/data_schema/aircraft/other/DT</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
</output>
@@ -213,14 +216,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -431,6 +434,9 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -752,6 +758,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
<parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -780,7 +789,7 @@
<workflow>
<problemDefinitionUID>unconverged-DOEJacobi</problemDefinitionUID>
<dataGraph>
- <name>XDSM - unconverged-DOE-J - Mdao</name>
+ <name>XDSM - unconverged-DOE-J-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -794,6 +803,10 @@
<fromParameterUID>/data_schema/aircraft/other/sigma1</fromParameterUID>
<toExecutableBlockUID>C[sigmas]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <toExecutableBlockUID>DOE</toExecutableBlockUID>
+ </edge>
<edge>
<fromExecutableBlockUID>C[sigmas]</fromExecutableBlockUID>
<toParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</toParameterUID>
@@ -826,6 +839,10 @@
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
@@ -848,51 +865,51 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/h</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma5</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma3</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma1</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/AR</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma2</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/Sref</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
+ <toParameterUID>/data_schema/reference/h</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
@@ -904,24 +921,28 @@
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/reference/M</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/geometry/tc</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/lambda</toParameterUID>
+ <toParameterUID>/data_schema/aircraft/other/Cf</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/objectives/R</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
- <toParameterUID>/data_schema/aircraft/geometry/section</toParameterUID>
+ <toParameterUID>/data_schema/reference/M</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Lambda</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>DOE</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/propulsion/Temp</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>DOE</fromExecutableBlockUID>
<toParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/dpdx</toParameterUID>
@@ -974,6 +995,10 @@
<fromExecutableBlockUID>Aerodynamics[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc</fromParameterUID>
<toExecutableBlockUID>DOE</toExecutableBlockUID>
@@ -1155,7 +1180,7 @@
<toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
</edge>
<edge>
- <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref</fromParameterUID>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>DOE</toExecutableBlockUID>
</edge>
<edge>
@@ -1361,7 +1386,7 @@
</edges>
</dataGraph>
<processGraph>
- <name>XDSM - unconverged-DOE-J - Mdao</name>
+ <name>XDSM - unconverged-DOE-J-CT - Mdao</name>
<edges>
<edge>
<fromExecutableBlockUID>F[R]</fromExecutableBlockUID>
@@ -1571,6 +1596,10 @@
<relatedParameterUID>/data_schema/aircraft/geometry/lambda</relatedParameterUID>
<label>DOE_lambda_{inp}</label>
</doeInputSampleList>
+ <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
+ <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
+ <label>DOE_Sref_{inp}</label>
+ </doeInputSampleList>
<doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/tc">
<relatedParameterUID>/data_schema/aircraft/geometry/tc</relatedParameterUID>
<label>DOE_tc_{inp}</label>
@@ -1587,10 +1616,6 @@
<relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
<label>DOE_T_{inp}</label>
</doeInputSampleList>
- <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/Sref">
- <relatedParameterUID>/data_schema/aircraft/geometry/Sref</relatedParameterUID>
- <label>DOE_Sref_{inp}</label>
- </doeInputSampleList>
<doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
<relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
<label>DOE_M_{inp}</label>
@@ -1609,6 +1634,10 @@
</doeInputSampleList>
</doeInputSampleLists>
<doeOutputSampleLists>
+ <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
+ <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
+ <label>DOE_WE_{out}</label>
+ </doeOutputSampleList>
<doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/sigmas/sigma4">
<relatedParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma4</relatedParameterUID>
<label>DOE_sigma4_{out}</label>
@@ -1665,6 +1694,7 @@
<doe uID="DOE">
<label>DOE</label>
<settings>
+ <doeMethod>Custom design table</doeMethod>
<doeTable>
<tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
<tableElement experimentID="0">0.1</tableElement>
@@ -1787,7 +1817,6 @@
<tableElement experimentID="9">1.6</tableElement>
</tableRow>
</doeTable>
- <doeMethod>Custom design table</doeMethod>
</settings>
<designVariables>
<designVariable>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
index 01f4f36c1e065c6c4a6c3a59a4c3d03866add225..1c343f3a437731acb43bb2dea5cea4ff50ab4f35 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -51,6 +51,9 @@
<output>
<parameterUID>/data_schema/aircraft/other/DT</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
</output>
@@ -216,14 +219,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -422,6 +425,9 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -530,6 +536,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -583,6 +592,10 @@
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
@@ -799,6 +812,10 @@
<fromParameterUID>/data_schema/aircraft/weight/WO</fromParameterUID>
<toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
index 956489bc99400242863d3274b4984b0ec3e46064..97dd25d01e7152ff6dc4284d4f99037737bd7fb7 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
@@ -3,14 +3,14 @@
<header>
<creator>Imco van Gent</creator>
<description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a mdao data graph (MDG).</modification>
<creator>Imco van Gent</creator>
- <timestamp>2018-03-15T17:18:43.703184</timestamp>
+ <timestamp>2018-03-21T15:55:30.252183</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -51,6 +51,9 @@
<output>
<parameterUID>/data_schema/aircraft/other/DT</parameterUID>
</output>
+ <output>
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </output>
<output>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
</output>
@@ -213,14 +216,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
@@ -425,6 +428,9 @@
<parameter uID="/data_schema/aircraft/weight/WO">
<label>WO</label>
</parameter>
+ <parameter uID="/data_schema/aircraft/weight/WE">
+ <label>WE</label>
+ </parameter>
<parameter uID="/data_schema/aircraft/weight/WF">
<label>WF</label>
</parameter>
@@ -524,6 +530,9 @@
<stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
</stateVariable>
+ <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
+ <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
+ </stateVariable>
<stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/ESF">
<parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
</stateVariable>
@@ -577,6 +586,10 @@
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
+ <edge>
+ <fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
+ <toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
+ </edge>
<edge>
<fromExecutableBlockUID>Propulsion[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
@@ -789,6 +802,10 @@
<fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/D</fromParameterUID>
<toExecutableBlockUID>Propulsion[main][1][1.0]</toExecutableBlockUID>
</edge>
+ <edge>
+ <fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
+ <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+ </edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>Performance[main][1][1.0]</toExecutableBlockUID>
diff --git a/examples/scripts/ssbj/CMDOWS/RCG.xml b/examples/scripts/ssbj/CMDOWS/RCG.xml
index e1e70cf94a68a2094880ad50cf1a89afac8b776e..4a96400314cc5056f91c28bbfba0f0d0c723b7a0 100644
--- a/examples/scripts/ssbj/CMDOWS/RCG.xml
+++ b/examples/scripts/ssbj/CMDOWS/RCG.xml
@@ -3,14 +3,14 @@
<header>
<creator>Lukas Mueller</creator>
<description>RCG CMDOWS file of the super-sonic business jet test case optimization problem</description>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
<updates>
<update>
<modification>KADMOS export of a repository connectivity graph (RCG).</modification>
<creator>Lukas Mueller</creator>
- <timestamp>2018-03-15T17:14:58.042549</timestamp>
+ <timestamp>2018-03-21T17:24:43.698182</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
@@ -222,14 +222,14 @@
<inputs>
<input>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
- <equationLabel>dpdx</equationLabel>
+ <equationLabel>R</equationLabel>
</input>
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
<equations uID="F[R]_equation">
- <equation language="Python">-dpdx</equation>
+ <equation language="Python">-R</equation>
</equations>
</output>
</outputs>
diff --git a/examples/scripts/ssbj/KDMS/FPG_MDA.kdms b/examples/scripts/ssbj/KDMS/FPG_MDA.kdms
index ab5d475f959bbfb9cc32be4b3247fa7c87e33058..50f5a76de51ba24b7ad28a0e0e271c5c0dddc76d 100644
Binary files a/examples/scripts/ssbj/KDMS/FPG_MDA.kdms and b/examples/scripts/ssbj/KDMS/FPG_MDA.kdms differ
diff --git a/examples/scripts/ssbj/KDMS/FPG_MDO.kdms b/examples/scripts/ssbj/KDMS/FPG_MDO.kdms
index 244b98f97ce78eb4af62151dd43f5b76097cddc1..6a2a3a48d25abadc31e1bed989b7c00816dc19fb 100644
Binary files a/examples/scripts/ssbj/KDMS/FPG_MDO.kdms and b/examples/scripts/ssbj/KDMS/FPG_MDO.kdms differ
diff --git a/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms b/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
index 086bb998364b9764e792afa965dd973137e9a75a..b4d0a532ddbfc189b91c97f3444fd06ca60c0e51 100644
--- a/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
+++ b/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
@@ -11,81 +11,80 @@ BLISS-2000q Ucoupled_functions_groupsq ]q (]q ha]q ha]q!haeUfunction_orderi
Structuresqm}qnsU&/data_schema/mdo_data/constraints/dpdxqo}qph}qqhR}qrhTUdpdx/1.0qssssU/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/other/finqt}quhJ}qvsU/data_schema/architectureNodes/initialGuessDesignVariables/data_schemaCopy/distributedArchitectures/group1/couplingWeights/w2__i2qw}qxh_}qysUW/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WEqz}q{U 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diff --git a/examples/scripts/ssbj/KDMS/Mdao_CO.kdms b/examples/scripts/ssbj/KDMS/Mdao_CO.kdms
index 9bfe103bab370b22e0d0d78ce6f943e558b52cb9..1f43289a1cf2ba371c8ee5102375a501d3b283d2 100644
--- a/examples/scripts/ssbj/KDMS/Mdao_CO.kdms
+++ b/examples/scripts/ssbj/KDMS/Mdao_CO.kdms
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diff --git a/examples/scripts/ssbj/KDMS/RCG.kdms b/examples/scripts/ssbj/KDMS/RCG.kdms
index bf1397596c2cdef8f6ca5dcadc18feb8d0243cd6..1fb26d319f3b579b3c5250fa641a58e1230aeb6f 100644
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diff --git a/examples/scripts/ssbj/VISTOMS/VISTOMS.html b/examples/scripts/ssbj/VISTOMS/VISTOMS.html
index 48630f8bcc9b5223ab62ae2570d42f7006c94dc1..023953353985789280264559eab099e64d4a098a 100644
--- a/examples/scripts/ssbj/VISTOMS/VISTOMS.html
+++ b/examples/scripts/ssbj/VISTOMS/VISTOMS.html
@@ -1879,7 +1879,7 @@ th, td {
}
//@Imco: Here is the sellar problem example data
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"name": "Lambda", "value": "unknown", "dimension": null}, {"level": 9, "type": "variable", "name": "tc__i2", "value": "unknown", "dimension": null}, {"level": 9, "type": "variable", "name": "Sref", "value": "unknown", "dimension": null}, {"level": 9, "type": "variable", "name": "AR__i2", "value": "unknown", "dimension": null}, {"level": 9, "type": "variable", "name": "Lambda__i2", "value": "unknown", "dimension": null}], "name": "geometry"}], "name": "aircraft"}, {"level": 7, "type": "variable", "children": [{"level": 8, "type": "variable", "name": "h__i2", "value": "unknown", "dimension": null}, {"level": 8, "type": "variable", "name": "M", "value": "unknown", "dimension": null}, {"level": 8, "type": "variable", "name": "h", "value": "unknown", "dimension": null}, {"level": 8, "type": "variable", "name": "M__i2", "value": "unknown", "dimension": null}], "name": "reference"}], "name": "data_schemaCopy"}], "name": "copyDesignVariables"}], "name": "architectureNodes"}, {"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "name": "h", "value": "unknown", "dimension": null}, {"level": 5, "type": "variable", "name": "M", "value": "unknown", "dimension": null}], "name": "reference"}], "name": "data_schemaCopy"}], "name": "finalDesignVariables"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "Theta", "value": "unknown", "dimension": null}], "name": "geometry"}, {"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "WF", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "WE", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "WT", "value": "unknown", "dimension": null}], "name": "weight"}, {"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "L", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "D", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "SFC", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "fin", "value": "unknown", "dimension": null}], "name": "other"}], "name": "aircraft"}, {"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "name": "ESF", "value": "unknown", "dimension": null}], "name": "reference"}], "name": "data_schemaCopy"}], "name": "couplingCopyVariables"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group2"}, {"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group0"}, {"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group1"}], "name": "distributedArchitectures"}, {"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "children": [{"level": 7, "type": "variable", "name": "DT", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "Temp", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "ESF", "value": "unknown", "dimension": null}], "name": "propulsion"}, {"level": 6, "type": "variable", "children": [{"level": 7, "type": "variable", "name": "sigma2", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "sigma5", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "sigma1", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "sigma4", "value": "unknown", "dimension": null}, {"level": 7, "type": "variable", "name": "sigma3", "value": "unknown", "dimension": null}], "name": "sigmas"}, {"level": 6, "type": "variable", "name": "Theta", "value": "unknown", "dimension": null}, {"level": 6, "type": "variable", "name": "dpdx", "value": "unknown", "dimension": null}], "name": "constraints"}, {"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "name": "R", "value": "unknown", "dimension": null}], "name": "objectives"}], "name": "mdo_data"}, {"level": 4, "type": "variable", "children": [{"level": 5, "type": "variable", "children": [{"level": 6, "type": "variable", "children": [{"level": 7, "type": "variable", "children": [{"level": 8, "type": "variable", "children": [{"level": 9, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group2"}, {"level": 8, "type": "variable", "children": [{"level": 9, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group0"}, {"level": 8, "type": "variable", "children": [{"level": 9, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group1"}], "name": "distributedArchitectures"}], "name": "data_schemaCopy"}], "name": "finalOutputVariables"}], "name": "architectureNodes"}], "name": "data_schemaCopy"}], "name": "finalOutputVariables"}], "name": "architectureNodes"}, {"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "name": "sigma3", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "sigma4", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "sigma5", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "sigma1", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "sigma2", "value": "unknown", "dimension": null}], "name": "sigmas"}, {"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "name": "ESF", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "DT", "value": "unknown", "dimension": null}, {"level": 4, "type": "variable", "name": "Temp", "value": "unknown", "dimension": null}], "name": "propulsion"}, {"level": 3, "type": "variable", "name": "Theta", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "dpdx", "value": "unknown", "dimension": null}], "name": "constraints"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "R", "value": "unknown", "dimension": null}], "name": "objectives"}], "name": "mdo_data"}, {"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "Theta", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "lambda", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "AR", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "tc", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "section", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "Lambda", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "Sref", "value": "unknown", "dimension": null}], "name": "geometry"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "WT", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "WO", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "WE", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "WF", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "WBE", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "WFO", "value": "unknown", "dimension": null}], "name": "weight"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "L", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "D", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "fin", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "T", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "sigma4", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "sigma3", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "sigma2", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "sigma1", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "Cf", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "Nz", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "dpdx", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "R", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "SFC", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "sigma5", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "CDmin", "value": "unknown", "dimension": null}, {"level": 3, "type": "variable", "name": "DT", "value": "unknown", "dimension": null}], "name": "other"}], "name": "aircraft"}, {"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group0"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group2"}, {"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "name": "objective", "value": "unknown", "dimension": null}], "name": "group1"}], "name": "distributedArchitectures"}, {"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "name": "ESF", "value": "unknown", "dimension": null}, {"level": 2, "type": "variable", "name": "h", "value": "unknown", "dimension": null}, {"level": 2, "type": "variable", "name": "Temp", "value": "unknown", "dimension": null}, {"level": 2, "type": "variable", "name": "M", "value": "unknown", "dimension": null}], "name": "reference"}]}}, "id": "06", "name": "XDSM - CO - Mdao"}], "categories": [{"name": "schema", "description": "schema"}, {"name": "catschema_nodeLev", "description": "node levels"}, {"name": "catschema_funLev", "description": "function levels"}, {"name": "catschema_roleLev", "description": "role levels"}, {"name": "catschema_sysLev", "description": "system levels"}]}
function loadAllData(data)
{
makeKadmosMenu(data);
diff --git a/examples/scripts/ssbj_mda.py b/examples/scripts/ssbj_mda.py
index 9a774fe52693f7602ad579d132de0fdd0156098b..21c895d591af98be0a58a1496fafe1a4603c8ab4 100644
--- a/examples/scripts/ssbj_mda.py
+++ b/examples/scripts/ssbj_mda.py
@@ -14,14 +14,17 @@ mdao_definitions = ['unconverged-MDA-GS', # 0
'unconverged-MDA-J', # 1
'converged-MDA-GS', # 2
'converged-MDA-J', # 3
- 'unconverged-DOE-GS', # 4
- 'unconverged-DOE-J', # 5
- 'converged-DOE-GS', # 6
- 'converged-DOE-J'] # 7
+ 'unconverged-DOE-GS-CT', # 4
+ 'unconverged-DOE-J-CT', # 5
+ 'converged-DOE-GS-CT', # 6
+ 'converged-DOE-J-CT', # 7
+ 'converged-DOE-GS-FF', # 8
+ 'converged-DOE-GS-LH', # 9
+ 'converged-DOE-GS-MC'] # 10
# Settings for scripting
mdao_definitions_loop_all = True # Option for looping through all MDAO definitions
-mdao_definition_id = 0 # Option for selecting a MDAO definition (in case mdao_definitions_loop_all=False)
+mdao_definition_id = 6 # Option for selecting a MDAO definition (in case mdao_definitions_loop_all=False)
# Settings for loading and saving
kb_dir = os.path.join(os.path.dirname(os.path.realpath(__file__)), '../knowledgebases')
@@ -30,7 +33,7 @@ cmdows_dir = 'ssbj/CMDOWS'
kdms_dir = 'ssbj/KDMS'
vistoms_dir = 'ssbj/VISTOMS'
-print 'Loading repository connectivity graph...'
+print('Loading repository connectivity graph...')
rcg = load(os.path.join(kdms_dir, 'RCG.kdms'))
function_order = ['Structures', 'Aerodynamics', 'Propulsion', 'Performance',
@@ -62,27 +65,14 @@ fpg.mark_as_qois([nd for nd in rcg.find_all_nodes(category='variable') if '/mdo_
fpg.mark_as_qois([nd for nd in rcg.find_all_nodes(category='variable') if '/mdo_data/constraints/propulsion/DT' in nd])
fpg.mark_as_qois([nd for nd in rcg.find_all_nodes(category='variable') if '/mdo_data/constraints/propulsion/Temp' in nd])
+# Add WE as QOI for testing with RCE
+fpg.mark_as_qois([nd for nd in rcg.find_all_nodes(category='variable') if '/aircraft/weight/WE' in nd])
+
# Search for problem roles
fpg.add_function_problem_roles()
-# Create a DSM visualization of the FPG
-fpg.create_dsm(file_name='FPG_' + architecture_type, function_order=function_order, include_system_vars=True,
- destination_folder=pdf_dir)
-# Create a VISTOMS visualization of the FPG (and add it to the existing directory)
-fpg.vistoms_add(vistoms_dir, function_order=function_order)
-
-# Save the FPG as kdms
-fpg.save('FPG_' + architecture_type, destination_folder=kdms_dir)
-# Save the FPG as cmdows (and do an integrity check)
-fpg.save('FPG_' + architecture_type, file_type='cmdows', destination_folder=cmdows_dir,
- description='FPG CMDOWS file of the super-sonic business jet test case optimization problem',
- creator='Imco van Gent',
- version='0.1',
- pretty_print=True,
- integrity=True)
-
for mdao_definition in mdao_definitions:
- print 'Scripting ' + str(mdao_definition) + '...'
+ print('Scripting ' + str(mdao_definition) + '...')
# If DOE, assign design variables
if 'DOE' in mdao_definition:
@@ -101,11 +91,48 @@ for mdao_definition in mdao_definitions:
lower_bounds=[ds_vr[1] for ds_vr in des_vars],
nominal_values=[ds_vr[2] for ds_vr in des_vars],
upper_bounds=[ds_vr[3] for ds_vr in des_vars],
- samples=[list(np.linspace(ds_vr[1], ds_vr[2], n_samples)) for ds_vr in des_vars])
+ samples=[list(np.linspace(ds_vr[1], ds_vr[2], n_samples)) for ds_vr in
+ des_vars] if '-CT' in mdao_definition else None)
# Change the problem formulation of the FPG based on the MDAO definition
+ if 'DOE' in mdao_definition:
+ doe_settings = dict()
+ if mdao_definition.endswith('-CT'):
+ doe_settings['doe_method'] = 'Custom design table'
+ elif mdao_definition.endswith('-FF'):
+ doe_settings['doe_method'] = 'Full factorial design'
+ doe_settings['doe_runs'] = 2
+ elif mdao_definition.endswith('-LH'):
+ doe_settings['doe_method'] = 'Latin hypercube design'
+ doe_settings['doe_seed'] = 5
+ doe_settings['doe_runs'] = 20
+ elif mdao_definition.endswith('-MC'):
+ doe_settings['doe_method'] = 'Monte Carlo design'
+ doe_settings['doe_seed'] = 9
+ doe_settings['doe_runs'] = 10
+ else:
+ raise AssertionError('Could not determine the doe_method.')
+ else:
+ doe_settings = None
+
fpg.add_problem_formulation(mdao_definition, function_order,
- doe_settings={'doe_method':'Custom design table'} if 'DOE' in mdao_definition else None)
+ doe_settings=doe_settings)
+
+ # Create a DSM visualization of the FPG
+ fpg.create_dsm(file_name='FPG_' + architecture_type, function_order=function_order, include_system_vars=True,
+ destination_folder=pdf_dir)
+ # Create a VISTOMS visualization of the FPG (and add it to the existing directory)
+ fpg.vistoms_add(vistoms_dir, function_order=function_order)
+
+ # Save the FPG as kdms
+ fpg.save('FPG_' + architecture_type, destination_folder=kdms_dir)
+ # Save the FPG as cmdows (and do an integrity check)
+ fpg.save('FPG_' + architecture_type, file_type='cmdows', destination_folder=cmdows_dir,
+ description='FPG CMDOWS file of the super-sonic business jet test case optimization problem',
+ creator='Imco van Gent',
+ version='0.1',
+ pretty_print=True,
+ integrity=True)
# Get Mdao graphs
mdg, mpg = fpg.impose_mdao_architecture()
diff --git a/kadmos/graph/graph_data.py b/kadmos/graph/graph_data.py
index 78065c4dbd025d4af216024ac1fe3cbf6305b3f9..4a4c6eecee9c00f5e4ad6f2bfe76443fc3d9629a 100644
--- a/kadmos/graph/graph_data.py
+++ b/kadmos/graph/graph_data.py
@@ -2617,9 +2617,9 @@ class FundamentalProblemGraph(DataGraph, KeChainMixin):
if doe_settings:
self.graph['problem_formulation']['doe_settings'] = dict()
self.graph['problem_formulation']['doe_settings']['doe_method'] = doe_settings['doe_method']
- if 'doe_seed' in self.graph['problem_formulation']['doe_settings']:
+ if 'doe_seed' in doe_settings:
self.graph['problem_formulation']['doe_settings']['doe_seed'] = doe_settings['doe_seed']
- if 'doe_runs' in self.graph['problem_formulation']['doe_settings']:
+ if 'doe_runs' in doe_settings:
self.graph['problem_formulation']['doe_settings']['doe_runs'] = doe_settings['doe_runs']
def partition_graph(self, n_parts, include_run_time=False, tpwgts=None, recursive=True, contig=False):
@@ -4124,6 +4124,11 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
graph_settings = self.node[graph_node].get('settings')
if graph_settings is not None:
cmdows_settings = cmdows_executable_block_elem.add('settings')
+ cmdows_settings.add('doeMethod', graph_settings.get('doe_method'))
+ if graph_settings.get('doe_runs') is not None:
+ cmdows_settings.add('doeRuns', graph_settings.get('doe_runs'))
+ if graph_settings.get('doe_seed') is not None:
+ cmdows_settings.add('doeSeed', graph_settings.get('doe_seed'))
if graph_settings.get('doe_table') is not None: # TODO: Temp fix, doe should always have settings
cmdows_table = cmdows_settings.add('doeTable')
for graph_row_index, graph_row in enumerate(graph_settings.get('doe_table_order')):
@@ -4131,12 +4136,12 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
for graph_element_index, graph_element in enumerate(graph_settings.get('doe_table')):
cmdows_row.add('tableElement', graph_element[graph_row_index],
attrib={'experimentID': str(graph_element_index)})
- cmdows_settings.add('doeMethod', graph_settings.get('doe_method'))
graph_des_vars = [{'designVariableUID': self.PROBLEM_ROLES_VAR_SUFFIXES[0] + var} for var in
self.node[graph_node].get('design_variables')]
cmdows_executable_block_elem.add('designVariables', graph_des_vars)
else:
- cmdows_executable_block_elem.add('settings', self.node[graph_node].get('settings'))
+ cmdows_executable_block_elem.add('settings', self.node[graph_node].get('settings'),
+ camel_case_conversion=True)
# Create architectureElements/executableBlocks/...Analyses/...
architecture_roles_funs = np.setdiff1d(self.ARCHITECTURE_ROLES_FUNS, self.CMDOWS_ARCHITECTURE_ROLE_SPLITTER,
@@ -4261,7 +4266,12 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
architecture_role=self.ARCHITECTURE_ROLES_FUNS[1],
shape='8',
label=self.OPTIMIZER_LABEL,
- level=None)
+ settings={'algorithm': 'Dakota Quasi-Newton method',
+ 'maximum_iterations': 1000,
+ 'maximum_function_evaluations': 1000,
+ 'constraint_tolerance': 1e-4,
+ 'convergence_tolerance': 1e-4,
+ 'apply_scaling': True})
elif mdao_arch in self.OPTIONS_ARCHITECTURES[5:7]: # unc-DOE, con-DOE
assert not self.has_node(self.DOE_STRING), 'DOE name already in use in FPG.'
self.add_node(self.DOE_STRING,
@@ -4269,7 +4279,6 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
architecture_role=self.ARCHITECTURE_ROLES_FUNS[3], # doe
shape='8',
label=self.DOE_LABEL,
- level=None,
settings=self.graph['problem_formulation']['doe_settings'])
# Add architecture role to post-iterator functions
functions = mg_function_ordering[self.FUNCTION_ROLES[4]]
@@ -4286,7 +4295,8 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
architecture_role=self.ARCHITECTURE_ROLES_FUNS[2],
shape='8',
label=self.CONVERGER_LABEL,
- level=None)
+ settings={'convergence_tolerance_absolute': 1e-6, 'convergence_tolerance_relative': 1e-6,
+ 'last_iterations_to_consider': 1, 'maximum_iterations': 100})
# Add local convergers if needed
if local_convergers:
@@ -4297,7 +4307,8 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
architecture_role=self.ARCHITECTURE_ROLES_FUNS[2],
shape='8',
label=self.CONVERGER_LABEL + str(converger),
- level=None)
+ settings={'tolerance_absolute': 1e-6, 'tolerance_relative': 1e-6,
+ 'last_iterations_to_consider': 1, 'maximum_iterations': 100})
# Add architecture role to coupled functions
for func in mg_function_ordering[self.FUNCTION_ROLES[1]]:
@@ -4311,7 +4322,6 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
assert not self.has_node(self.CONSCONS_STRING), 'Consistency constraint name already in use in FPG.'
self.add_node(self.CONSCONS_STRING,
label=self.CONSCONS_LABEL,
- level=None,
shape='s',
category='function',
architecture_role=self.ARCHITECTURE_ROLES_FUNS[8])
@@ -4450,7 +4460,7 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
label=self.COF_LABEL + str(group_idx),
instance=1,
problem_role=self.FUNCTION_ROLES[2], # post-coupling
- architecture_role=self.ARCHITECTURE_ROLES_FUNS[9]) # consistency constraint function
+ architecture_role=self.ARCHITECTURE_ROLES_FUNS[4]) # post-coupling analysis
# Connect the variable inputs for the function
for idx, (var1, var2) in enumerate(ccv_mappings.iteritems()):
eq_lab1 = 'x{}_0'.format(idx)
@@ -4794,7 +4804,9 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
category='function',
architecture_role=self.ARCHITECTURE_ROLES_FUNS[2],
label=label,
- instance=1)
+ instance=1,
+ settings={'convergence_tolerance_absolute': 1e-6, 'convergence_tolerance_relative': 1e-6,
+ 'last_iterations_to_consider': 1, 'maximum_iterations': 100})
assert conv_type in self.OPTIONS_CONVERGERS + [self.OPTIONS_ARCHITECTURES[2]], \
'Invalid converger type %s specified.' % conv_type
assert isinstance(coupling_functions, list)
@@ -4841,7 +4853,13 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
category='function',
architecture_role=self.ARCHITECTURE_ROLES_FUNS[1],
label=label,
- instance=1)
+ instance=1,
+ settings = {'algorithm': 'Dakota Quasi-Newton method',
+ 'maximum_iterations': 1000,
+ 'maximum_function_evaluations': 1000,
+ 'constraint_tolerance': 1e-4,
+ 'convergence_tolerance': 1e-4,
+ 'apply_scaling': True})
assert isinstance(design_variable_nodes, list)
for des_var in design_variable_nodes:
assert self.has_node(des_var), 'Design variable %s is missing in the graph.' % des_var
@@ -4957,7 +4975,8 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
category='function',
architecture_role=self.ARCHITECTURE_ROLES_FUNS[3],
label=label,
- instance=1)
+ instance=1,
+ settings=self.graph['problem_formulation']['doe_settings'])
assert isinstance(design_variable_nodes, list)
for des_var in design_variable_nodes:
assert self.has_node(des_var), 'Design variable %s is missing in the graph.' % des_var
diff --git a/kadmos/utilities/general.py b/kadmos/utilities/general.py
index aed3a8b55aec1a212c76f94260ddb64ed77eb9b8..b07f2a86b456316f017e18509ab0af5e37729e1a 100644
--- a/kadmos/utilities/general.py
+++ b/kadmos/utilities/general.py
@@ -144,6 +144,9 @@ def get_mdao_setup(mdao_setup):
'distributed-convergence', # 16
'CO', # 17
'BLISS-2000'] # 18
+ if mdao_setup.endswith(('-FF', '-MC', '-LH', '-CT')):
+ mdao_setup = mdao_setup[:-3]
+
if mdao_setup == mdao_defintions[0]:
mdo_architecture = 'unconverged-MDA'
mda_type = None