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LR-FPP-MDO
KADMOS
Commits
82e78a41
Commit
82e78a41
authored
8 years ago
by
Andreas Makus
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adapted base file so that all Q3D, EMWET ins and outs are validated successfully
parent
2ac75b2d
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pyKADMOS/KB_CPACS/AGILE_DC1_L0_MDA-base.xml
+81
-40
81 additions, 40 deletions
pyKADMOS/KB_CPACS/AGILE_DC1_L0_MDA-base.xml
with
81 additions
and
40 deletions
pyKADMOS/KB_CPACS/AGILE_DC1_L0_MDA-base.xml
+
81
−
40
View file @
82e78a41
...
...
@@ -1959,11 +1959,11 @@
<ribsDefinition
uID=
"wing_ribs_inner"
>
<name>
wing_ribs
</name>
<ribsPositioning>
<ribReference>
wing_
Spar
_FS
</ribReference>
<ribReference>
front
Spar
</ribReference>
<etaStart>
0.0
</etaStart>
<etaEnd>
0.106761565836
</etaEnd>
<ribStart>
wing_
Spar
_FS
</ribStart>
<ribEnd>
wing_
Spar
_RS
</ribEnd>
<ribStart>
front
Spar
</ribStart>
<ribEnd>
rear
Spar
</ribEnd>
<numberOfRibs>
4
</numberOfRibs>
<ribCrossingBehaviour>
cross
</ribCrossingBehaviour>
<ribRotation>
...
...
@@ -1981,11 +1981,11 @@
<ribsDefinition
uID=
"wing_ribs_engine1"
>
<name>
wing_ribs
</name>
<ribsPositioning>
<ribReference>
wing_
Spar
_FS
</ribReference>
<ribReference>
front
Spar
</ribReference>
<etaStart>
0.163701067616
</etaStart>
<etaEnd>
0.286476868327
</etaEnd>
<ribStart>
wing_
Spar
_FS
</ribStart>
<ribEnd>
wing_
Spar
_RS
</ribEnd>
<ribStart>
front
Spar
</ribStart>
<ribEnd>
rear
Spar
</ribEnd>
<numberOfRibs>
3
</numberOfRibs>
<ribCrossingBehaviour>
cross
</ribCrossingBehaviour>
<ribRotation>
...
...
@@ -2003,11 +2003,11 @@
<ribsDefinition
uID=
"wing_ribs_engine2"
>
<name>
wing_ribs
</name>
<ribsPositioning>
<ribReference>
wing_
Spar
_FS
</ribReference>
<ribReference>
front
Spar
</ribReference>
<etaStart>
0.163701067616
</etaStart>
<etaEnd>
0.313523131673
</etaEnd>
<ribStart>
wing_
Spar
_FS
</ribStart>
<ribEnd>
wing_
Spar
_RS
</ribEnd>
<ribStart>
front
Spar
</ribStart>
<ribEnd>
rear
Spar
</ribEnd>
<numberOfRibs>
1
</numberOfRibs>
<ribCrossingBehaviour>
cross
</ribCrossingBehaviour>
<ribRotation>
...
...
@@ -2025,15 +2025,15 @@
<ribsDefinition
uID=
"wing_ribs_outer"
>
<name>
wing_ribs
</name>
<ribsPositioning>
<ribReference>
wing_
Spar
_FS
</ribReference>
<ribReference>
front
Spar
</ribReference>
<etaStart>
0.370462633452
</etaStart>
<etaEnd>
0.95
</etaEnd>
<ribStart>
wing_
Spar
_FS
</ribStart>
<ribEnd>
wing_
Spar
_RS
</ribEnd>
<ribStart>
front
Spar
</ribStart>
<ribEnd>
rear
Spar
</ribEnd>
<numberOfRibs>
11
</numberOfRibs>
<ribCrossingBehaviour>
end
</ribCrossingBehaviour>
<ribRotation>
<ribRotationReference>
wing_
Spar
_FS
</ribRotationReference>
<ribRotationReference>
front
Spar
</ribRotationReference>
<z>
90.
</z>
</ribRotation>
</ribsPositioning>
...
...
@@ -2047,43 +2047,43 @@
</ribsDefinitions>
<spars>
<sparPositions>
<sparPosition
uID=
"
wing_
Spar_
FS_
P0"
>
<sparPosition
uID=
"
front
Spar_P0"
>
<eta>
0.0
</eta>
<xsi>
0.1
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
FS_
P1"
>
<sparPosition
uID=
"
front
Spar_P1"
>
<eta>
0.106761565836
</eta>
<xsi>
0.1
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
FS_
P2"
>
<sparPosition
uID=
"
front
Spar_P2"
>
<eta>
1.0
</eta>
<xsi>
0.460829493088
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
RS_
P0"
>
<sparPosition
uID=
"
rear
Spar_P0"
>
<eta>
0.0
</eta>
<xsi>
0.56
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
RS_
P1"
>
<sparPosition
uID=
"
rear
Spar_P1"
>
<eta>
0.106761565836
</eta>
<xsi>
0.56
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
RS_
P2"
>
<sparPosition
uID=
"
rear
Spar_P2"
>
<eta>
0.350213340505
</eta>
<xsi>
0.6
</xsi>
</sparPosition>
<sparPosition
uID=
"
wing_
Spar_
RS_
P3"
>
<sparPosition
uID=
"
rear
Spar_P3"
>
<eta>
1.0
</eta>
<xsi>
0.59
</xsi>
</sparPosition>
</sparPositions>
<sparSegments>
<sparSegment
uID=
"
wing_
Spar
_FS
"
>
<name>
wing_
Spar
_FS
</name>
<description>
wing_
Spar
_FS
</description>
<sparSegment
uID=
"
front
Spar"
>
<name>
front
Spar
</name>
<description>
front
Spar
</description>
<sparPositionUIDs>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
FS_
P0
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
FS_
P1
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
FS_
P2
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
front
Spar_P0
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
front
Spar_P1
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
front
Spar_P2
</sparPositionUID>
</sparPositionUIDs>
<sparCrossSection>
<upperCap>
...
...
@@ -2110,14 +2110,14 @@
<rotation>
90.0
</rotation>
</sparCrossSection>
</sparSegment>
<sparSegment
uID=
"
wing_
Spar
_RS
"
>
<name>
wing_
Spar
_RS
</name>
<description>
wing_
Spar
_RS
</description>
<sparSegment
uID=
"
rear
Spar"
>
<name>
rear
Spar
</name>
<description>
rear
Spar
</description>
<sparPositionUIDs>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
RS_
P0
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
RS_
P1
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
RS_
P2
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
wing_
Spar_
RS_
P3
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
rear
Spar_P0
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
rear
Spar_P1
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
rear
Spar_P2
</sparPositionUID>
<sparPositionUID
isLink=
"True"
>
rear
Spar_P3
</sparPositionUID>
</sparPositionUIDs>
<sparCrossSection>
<upperCap>
...
...
@@ -3320,14 +3320,14 @@
<name>
wing_tank_inner
</name>
<geometry>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_FS
</sparUID>
<sparUID
isLink=
"True"
>
front
Spar
</sparUID>
</border>
<border>
<ribDefinitionUID
isLink=
"True"
>
wing_ribs_inner
</ribDefinitionUID>
<ribNumber>
4
</ribNumber>
</border>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_RS
</sparUID>
<sparUID
isLink=
"True"
>
rear
Spar
</sparUID>
</border>
</geometry>
</wingFuelTank>
...
...
@@ -3339,14 +3339,14 @@
<ribNumber>
4
</ribNumber>
</border>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_FS
</sparUID>
<sparUID
isLink=
"True"
>
front
Spar
</sparUID>
</border>
<border>
<ribDefinitionUID
isLink=
"True"
>
wing_ribs_engine2
</ribDefinitionUID>
<ribNumber>
1
</ribNumber>
</border>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_RS
</sparUID>
<sparUID
isLink=
"True"
>
rear
Spar
</sparUID>
</border>
</geometry>
</wingFuelTank>
...
...
@@ -3358,14 +3358,14 @@
<ribNumber>
1
</ribNumber>
</border>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_FS
</sparUID>
<sparUID
isLink=
"True"
>
front
Spar
</sparUID>
</border>
<border>
<ribDefinitionUID
isLink=
"True"
>
wing_ribs_outer
</ribDefinitionUID>
<ribNumber>
8
</ribNumber>
</border>
<border>
<sparUID
isLink=
"True"
>
wing_
Spar
_RS
</sparUID>
<sparUID
isLink=
"True"
>
rear
Spar
</sparUID>
</border>
</geometry>
</wingFuelTank>
...
...
@@ -4523,7 +4523,10 @@
</massDescription>
</mFuselageStructure>
</mFuselagesStructure>
<mWingsStructure>
<mWingsStructure>
<massDescription>
<mass>
3123.1
</mass>
</massDescription>
<mWingStructure>
<massDescription>
<mass>
4856.32744539
</mass>
...
...
@@ -4933,6 +4936,9 @@
<engine
uID=
"engine"
>
<description>
AGILE DC-1 Reference Engine 1
</description>
<analysis>
<mass>
<mass>
2266.0
</mass>
</mass>
<bpr00>
4.4
</bpr00>
<thrust00>
61367.6832837
</thrust00>
</analysis>
...
...
@@ -4940,8 +4946,22 @@
<diameter>
1.40118975114
</diameter>
<length>
2.41986362808
</length>
</geometry>
<transformation>
<translation
refType=
"absLocal"
>
<x>
13.6765
</x>
<y>
5.7482
</y>
<z>
-2.33895
</z>
</translation>
</transformation>
</engine>
</engines>
<materials>
<material
uID=
"aluminium2024"
>
<rho>
2.8e3
</rho>
<k11>
80.9561216474e9
</k11>
<sig11>
0.3268e9
</sig11>
</material>
</materials>
</vehicles>
<toolspecific>
<q3D>
...
...
@@ -4953,5 +4973,26 @@
<Q3D.n_wing>
8
</Q3D.n_wing>
<flightLoadCaseUID>
Design-maneuver-speed_2.5g_F0_MTOM_max_fuel_12000m
</flightLoadCaseUID>
</q3D>
<EMWET
uID=
"EMWET"
>
<wingUID>
MainWing_wingID
</wingUID>
<loadcaseUID>
Design-maneuver-speed_2.5g_F0_MTOM_max_fuel_12000m
</loadcaseUID>
<preferences>
<preference_description>
"model" to obtain from model, "given" to take given value
</preference_description>
<spar_pref>
model
</spar_pref>
<fueltank_pref>
given
</fueltank_pref>
<rib_pref>
model
</rib_pref>
</preferences>
<spars>
<spar_start_x>
0.2
</spar_start_x>
<spar_end_x>
0.8
</spar_end_x>
</spars>
<fueltank>
<fueltank_start_y>
0.1
</fueltank_start_y>
<fueltank_end_y>
0.7
</fueltank_end_y>
</fueltank>
<stringer_efficiency>
0.96
</stringer_efficiency>
<ribpitch>
0.5
</ribpitch>
<display>
0
</display>
</EMWET>
</toolspecific>
</cpacs>
\ No newline at end of file
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