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add deprecated cpacsVersion node to allow files to be opened in TiGL …
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -1,115 +1,116 @@ | ||
| <cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="../schema/cpacs_schema.xsd"> | ||
| <header> | ||
| <name>Fuel tank examples</name> | ||
| <version>1.0.0</version> | ||
| <!-- <cpacsVersion>3.4</cpacsVersion> --> | ||
| <versionInfos> | ||
| <versionInfo version="1.0.0"> | ||
| <creator>DLR-SL</creator> | ||
| <timestamp>2022-11-30T11:56:46.259694</timestamp> | ||
| <description>Some examples how to parametrize fuel tanks</description> | ||
| <cpacsVersion>3.4</cpacsVersion> | ||
| </versionInfo> | ||
| </versionInfos> | ||
| </header> | ||
| <vehicles> | ||
| <aircraft> | ||
| <model uID="aircraftModel"> | ||
| <name>Aircraft</name> | ||
| <fuselages> | ||
| <fuselage uID="fuselage"> | ||
| <name>Main fuselage</name> | ||
| <transformation /> | ||
| <sections> | ||
| <section uID="sec1"> | ||
| <name>Section1</name> | ||
| <transformation /> | ||
| <elements> | ||
| <element uID="sec1el1"> | ||
| <name>Section 1 Element 1</name> | ||
| <profileUID>fuselageCircleProfile</profileUID> | ||
| <transformation /> | ||
| </element> | ||
| </elements> | ||
| </section> | ||
| <section uID="sec2"> | ||
| <name>Section2</name> | ||
| <transformation /> | ||
| <elements> | ||
| <element uID="sec2el1"> | ||
| <name>Section 2 Element 1</name> | ||
| <profileUID>fuselageCircleProfile</profileUID> | ||
| <transformation /> | ||
| </element> | ||
| </elements> | ||
| </section> | ||
| </sections> | ||
| <positionings> | ||
| <positioning uID="sec2positioning"> | ||
| <name>Section 2 positioning</name> | ||
| <length>10</length> | ||
| <sweepAngle>90</sweepAngle> | ||
| <dihedralAngle>0</dihedralAngle> | ||
| <toSectionUID>sec2</toSectionUID> | ||
| </positioning> | ||
| </positionings> | ||
| <segments> | ||
| <segment uID="seg1"> | ||
| <name>Segment 1</name> | ||
| <fromElementUID>sec1el1</fromElementUID> | ||
| <toElementUID>sec2el1</toElementUID> | ||
| </segment> | ||
| </segments> | ||
| <fuelTanks> | ||
| <genericFuelTanks> | ||
| <genericFuelTank uID="simpleTank"> | ||
| <name>Cryogenic fuel tank</name> | ||
| <designParameters> | ||
| <transformation> | ||
| <translation> | ||
| <x>10.</x> | ||
| <y>2.</y> | ||
| <z>0.</z> | ||
| </translation> | ||
| </transformation> | ||
| <cylinderRadius>1.</cylinderRadius> | ||
| <cylinderLength>5.</cylinderLength> | ||
| <domeType> | ||
| <spherical/> | ||
| </domeType> | ||
| <material> | ||
| <materialUID>mat1</materialUID> | ||
| </material> | ||
| </designParameters> | ||
| </genericFuelTank> | ||
| </genericFuelTanks> | ||
| </fuelTanks> | ||
| </fuselage> | ||
| </fuselages> | ||
| </model> | ||
| </aircraft> | ||
| <profiles> | ||
| <fuselageProfiles> | ||
| <fuselageProfile uID="fuselageCircleProfile"> | ||
| <name>Circle</name> | ||
| <description>Profile build up from set of Points on Circle where may Dimensions are 1..-1</description> | ||
| <pointList> | ||
| <x mapType="vector">0.0;0.0;0.0;0.0;0.0</x> | ||
| <y mapType="vector">0.0;1.0;0.0;-1.0;0.0</y> | ||
| <z mapType="vector">1.0;0.0;-1.0;0.0;1.0</z> | ||
| </pointList> | ||
| </fuselageProfile> | ||
| </fuselageProfiles> | ||
| </profiles> | ||
| <materials> | ||
| <material uID="mat1"> | ||
| <name>Material 1</name> | ||
| <description>This is a dummy material</description> | ||
| <rho>1.234</rho> | ||
| <isotropicProperties> | ||
| <E>1.234</E> | ||
| </isotropicProperties> | ||
| </material> | ||
| </materials> | ||
| </vehicles> | ||
| <cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="../schema/cpacs_schema.xsd"> | ||
| <header> | ||
| <name>Fuel tank examples</name> | ||
| <version>1.0.0</version> | ||
| <!-- Deprecated: The <cpacsVersion> is needed to open the file in TiGL. TiGL will soon be adapted to get this information from the versinInfo node. --> | ||
| <cpacsVersion>3.5</cpacsVersion> | ||
| <versionInfos> | ||
| <versionInfo version="1.0.0"> | ||
| <creator>DLR-SL</creator> | ||
| <timestamp>2022-11-30T11:56:46.259694</timestamp> | ||
| <description>Some examples how to parametrize fuel tanks</description> | ||
| <cpacsVersion>3.4</cpacsVersion> | ||
| </versionInfo> | ||
| </versionInfos> | ||
| </header> | ||
| <vehicles> | ||
| <aircraft> | ||
| <model uID="aircraftModel"> | ||
| <name>Aircraft</name> | ||
| <fuselages> | ||
| <fuselage uID="fuselage"> | ||
| <name>Main fuselage</name> | ||
| <transformation /> | ||
| <sections> | ||
| <section uID="sec1"> | ||
| <name>Section1</name> | ||
| <transformation /> | ||
| <elements> | ||
| <element uID="sec1el1"> | ||
| <name>Section 1 Element 1</name> | ||
| <profileUID>fuselageCircleProfile</profileUID> | ||
| <transformation /> | ||
| </element> | ||
| </elements> | ||
| </section> | ||
| <section uID="sec2"> | ||
| <name>Section2</name> | ||
| <transformation /> | ||
| <elements> | ||
| <element uID="sec2el1"> | ||
| <name>Section 2 Element 1</name> | ||
| <profileUID>fuselageCircleProfile</profileUID> | ||
| <transformation /> | ||
| </element> | ||
| </elements> | ||
| </section> | ||
| </sections> | ||
| <positionings> | ||
| <positioning uID="sec2positioning"> | ||
| <name>Section 2 positioning</name> | ||
| <length>10</length> | ||
| <sweepAngle>90</sweepAngle> | ||
| <dihedralAngle>0</dihedralAngle> | ||
| <toSectionUID>sec2</toSectionUID> | ||
| </positioning> | ||
| </positionings> | ||
| <segments> | ||
| <segment uID="seg1"> | ||
| <name>Segment 1</name> | ||
| <fromElementUID>sec1el1</fromElementUID> | ||
| <toElementUID>sec2el1</toElementUID> | ||
| </segment> | ||
| </segments> | ||
| <fuelTanks> | ||
| <genericFuelTanks> | ||
| <genericFuelTank uID="simpleTank"> | ||
| <name>Cryogenic fuel tank</name> | ||
| <designParameters> | ||
| <transformation> | ||
| <translation> | ||
| <x>10.</x> | ||
| <y>2.</y> | ||
| <z>0.</z> | ||
| </translation> | ||
| </transformation> | ||
| <cylinderRadius>1.</cylinderRadius> | ||
| <cylinderLength>5.</cylinderLength> | ||
| <domeType> | ||
| <spherical/> | ||
| </domeType> | ||
| <material> | ||
| <materialUID>mat1</materialUID> | ||
| </material> | ||
| </designParameters> | ||
| </genericFuelTank> | ||
| </genericFuelTanks> | ||
| </fuelTanks> | ||
| </fuselage> | ||
| </fuselages> | ||
| </model> | ||
| </aircraft> | ||
| <profiles> | ||
| <fuselageProfiles> | ||
| <fuselageProfile uID="fuselageCircleProfile"> | ||
| <name>Circle</name> | ||
| <description>Profile build up from set of Points on Circle where may Dimensions are 1..-1</description> | ||
| <pointList> | ||
| <x mapType="vector">0.0;0.0;0.0;0.0;0.0</x> | ||
| <y mapType="vector">0.0;1.0;0.0;-1.0;0.0</y> | ||
| <z mapType="vector">1.0;0.0;-1.0;0.0;1.0</z> | ||
| </pointList> | ||
| </fuselageProfile> | ||
| </fuselageProfiles> | ||
| </profiles> | ||
| <materials> | ||
| <material uID="mat1"> | ||
| <name>Material 1</name> | ||
| <description>This is a dummy material</description> | ||
| <rho>1.234</rho> | ||
| <isotropicProperties> | ||
| <E>1.234</E> | ||
| </isotropicProperties> | ||
| </material> | ||
| </materials> | ||
| </vehicles> | ||
| </cpacs> |
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