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Commit 2c4ecb21 authored by maaikedieuwertje's avatar maaikedieuwertje
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rerun 

Former-commit-id: 54eb44ad59f5d6c96ac26fdc90ec4ce06ec9e92d
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examples/scripts/ssbj/(X)DSM/RCG.pdf
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examples/scripts/ssbj/CMDOWS/RCG.xml
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......@@ -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>2018-02-24T18:06:50.816000</timestamp>
<timestamp>2018-02-28T09:42:08.896000</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>2018-02-24T18:06:50.816000</timestamp>
<timestamp>2018-02-28T09:42:08.896000</timestamp>
<fileVersion>0.1</fileVersion>
<cmdowsVersion>0.7</cmdowsVersion>
</update>
......@@ -47,61 +47,7 @@
</header>
<executableBlocks>
<designCompetences>
<designCompetence uID="structure[main][1][1.0]">
<ID>structure</ID>
<modeID>main</modeID>
<instanceID>1</instanceID>
<version>1.0</version>
<label>structure</label>
<metadata>
<generalInfo>
<owner>
<contactUID>remilafage</contactUID>
</owner>
<description>Weight estimation of different aircraft parts.</description>
<creator>
<contactUID>sylvaindubreuil</contactUID>
</creator>
</generalInfo>
</metadata>
</designCompetence>
<designCompetence uID="aerodynamics[main][1][1.0]">
<ID>aerodynamics</ID>
<modeID>main</modeID>
<instanceID>1</instanceID>
<version>1.0</version>
<label>aerodynamics</label>
<metadata>
<generalInfo>
<owner>
<contactUID>remilafage</contactUID>
</owner>
<description>Estimation of the aircraft lift and drag during cruise.</description>
<creator>
<contactUID>sylvaindubreuil</contactUID>
</creator>
</generalInfo>
</metadata>
</designCompetence>
<designCompetence uID="propulsion[main][1][1.0]">
<ID>propulsion</ID>
<modeID>main</modeID>
<instanceID>1</instanceID>
<version>1.0</version>
<label>propulsion</label>
<metadata>
<generalInfo>
<owner>
<contactUID>remilafage</contactUID>
</owner>
<description>Engine sizing and estimation of the engine thrust.</description>
<creator>
<contactUID>sylvaindubreuil</contactUID>
</creator>
</generalInfo>
</metadata>
</designCompetence>
<designCompetence uID="performance[main][1][1.0]">
<designCompetence uID="performance">
<ID>performance</ID>
<modeID>main</modeID>
<instanceID>1</instanceID>
......@@ -109,13 +55,10 @@
<label>performance</label>
<inputs>
<input>
<parameterUID>/data_schema/reference/h</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
<parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
<parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/other/L</parameterUID>
......@@ -132,11 +75,14 @@
<input>
<parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/other/Cf</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/geometry/tc</parameterUID>
<parameterUID>/data_schema/reference/h</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
......@@ -145,19 +91,19 @@
<parameterUID>/data_schema/reference/M</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/geometry/lambda</parameterUID>
<parameterUID>/data_schema/aircraft/geometry/Lambda</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/geometry/section</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/other/fin</parameterUID>
<parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/other/D</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
<parameterUID>/data_schema/aircraft/other/fin</parameterUID>
</input>
<input>
<parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
......@@ -168,43 +114,43 @@
</inputs>
<outputs>
<output>
<parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
<parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/L</parameterUID>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
</output>
<output>
<parameterUID>/data_schema/reference/ESF</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/SFC</parameterUID>
<parameterUID>/data_schema/aircraft/other/L</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/weight/WT</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
<parameterUID>/data_schema/aircraft/other/D</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/D</parameterUID>
<parameterUID>/data_schema/aircraft/other/fin</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/sigma</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
<parameterUID>/data_schema/reference/Temp</parameterUID>
</output>
<output>
<parameterUID>/data_schema/reference/Temp</parameterUID>
<parameterUID>/data_schema/aircraft/other/R</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/geometry/Theta</parameterUID>
<parameterUID>/data_schema/aircraft/other/dpdx</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/DT</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/other/fin</parameterUID>
<parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
</output>
<output>
<parameterUID>/data_schema/aircraft/weight/WF</parameterUID>
......@@ -327,131 +273,131 @@
<edges>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/section</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/Theta</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/AR</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>objective</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/objective</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Theta</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/reference/h</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/ESF</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/L</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WT</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/L</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/fin</toParameterUID>
</edge>
<edge>
<fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/sigma</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/Temp</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/L</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/ESF</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/dpdx</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/SFC</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WT</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WE</toParameterUID>
<fromExecutableBlockUID>performance</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/D</toParameterUID>
<fromParameterUID>/data_schema/aircraft/geometry/Sref</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/sigma</toParameterUID>
<fromParameterUID>/data_schema/aircraft/weight/WT</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
<fromParameterUID>/data_schema/reference/h</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/reference/Temp</toParameterUID>
<fromParameterUID>/data_schema/aircraft/weight/WE</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/geometry/Theta</toParameterUID>
<fromParameterUID>/data_schema/aircraft/weight/WF</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/DT</toParameterUID>
<fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/other/fin</toParameterUID>
<fromParameterUID>/data_schema/aircraft/other/L</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromExecutableBlockUID>performance[main][1][1.0]</fromExecutableBlockUID>
<toParameterUID>/data_schema/aircraft/weight/WF</toParameterUID>
<fromParameterUID>/data_schema/reference/ESF</fromParameterUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/SFC</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/Cf</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/reference/M</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/geometry/Lambda</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
......@@ -459,11 +405,11 @@
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/fin</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
<edge>
<fromParameterUID>/data_schema/aircraft/other/T</fromParameterUID>
<toExecutableBlockUID>performance[main][1][1.0]</toExecutableBlockUID>
<toExecutableBlockUID>performance</toExecutableBlockUID>
</edge>
</edges>
</dataGraph>
......
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