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MSBuild.exe .\documentation\Cpacs_doc_project.shfbproj | ||
REM for first time user, first unzip the file *development/3rdparty.zip*! | ||
REM potentially remove path to installed SandCastle from environment variable as the build might not success. | ||
|
||
MSBuild.exe .\documentation\Cpacs_doc_project.shfbproj |
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<?xml version="1.0" encoding="UTF-8"?> | ||
<cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" | ||
xsi:noNamespaceSchemaLocation="../schema/cpacs_schema.xsd"> | ||
<header> | ||
<name>Basic Wing Model</name> | ||
<creator>Marko Alder</creator> | ||
<timestamp>2019-12-04T10:30:00</timestamp> | ||
<version>1.0</version> | ||
<cpacsVersion>3.2</cpacsVersion> | ||
</header> | ||
<vehicles> | ||
<aircraft> | ||
<model uID="aircraft"> | ||
<name>aircraft</name> | ||
<wings> | ||
<wing uID="wing1"> | ||
<name>main wing</name> | ||
<transformation/> | ||
<sections> | ||
<section uID="wing1section1"> | ||
<name>root section</name> | ||
<transformation> | ||
<rotation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</rotation> | ||
<scaling> | ||
<x>1</x> | ||
<y>1</y> | ||
<z>1</z> | ||
</scaling> | ||
<translation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</translation> | ||
</transformation> | ||
<elements> | ||
<element uID="wing1section1element1"> | ||
<name>wing root element</name> | ||
<airfoilUID>NACA0009</airfoilUID> | ||
<transformation> | ||
<rotation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</rotation> | ||
<scaling> | ||
<x>1</x> | ||
<y>1</y> | ||
<z>1</z> | ||
</scaling> | ||
<translation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</translation> | ||
</transformation> | ||
</element> | ||
</elements> | ||
</section> | ||
<section uID="wing1section2"> | ||
<name>tip section</name> | ||
<transformation> | ||
<rotation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</rotation> | ||
<scaling> | ||
<x>1</x> | ||
<y>1</y> | ||
<z>1</z> | ||
</scaling> | ||
<translation> | ||
<x>0.5</x> | ||
<y>1.0</y> | ||
<z>0.0</z> | ||
</translation> | ||
</transformation> | ||
<elements> | ||
<element uID="wing1section2element1"> | ||
<name>wing tip element</name> | ||
<airfoilUID>NACA0009</airfoilUID> | ||
<transformation> | ||
<rotation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</rotation> | ||
<scaling> | ||
<x>0.5</x> | ||
<y>1</y> | ||
<z>0.5</z> | ||
</scaling> | ||
<translation> | ||
<x>0.0</x> | ||
<y>0.0</y> | ||
<z>0.0</z> | ||
</translation> | ||
</transformation> | ||
</element> | ||
</elements> | ||
</section> | ||
</sections> | ||
<segments> | ||
<segment uID="wing1segment1"> | ||
<name>wing segment</name> | ||
<fromElementUID>wing1section1element1</fromElementUID> | ||
<toElementUID>wing1section2element1</toElementUID> | ||
</segment> | ||
</segments> | ||
</wing> | ||
</wings> | ||
</model> | ||
</aircraft> | ||
<profiles> | ||
<wingAirfoils> | ||
<wingAirfoil uID="NACA0009"> | ||
<name>NACA0009 Airfoil</name> | ||
<description>NACA 4-digit symmetrical airfoil with a thickness of 9percent</description> | ||
<pointList> | ||
<x mapType="vector">1.0;0.99572;0.98296;0.96194;0.93301;0.89668;0.85355;0.80438;0.75;0.69134;0.62941;0.56526;0.5;0.43474;0.37059;0.33928;0.30866;0.27886;0.25;0.22221;0.19562;0.17033;0.14645;0.12408;0.10332;0.08427;0.06699;0.05156;0.03806;0.02653;0.01704;0.00961;0.00428;0.00107;0.0;0.00107;0.00428;0.00961;0.01704;0.02653;0.03806;0.05156;0.06699;0.08427;0.10332;0.12408;0.14645;0.17033;0.19562;0.22221;0.25;0.27886;0.30866;0.33928;0.37059;0.43474;0.5;0.56526;0.62941;0.69134;0.75;0.80438;0.85355;0.89668;0.93301;0.96194;0.98296;0.99572;1.0</x> | ||
<y mapType="vector">0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0;0.0</y> | ||
<z mapType="vector">0.0;0.00057;0.00218;0.00463;0.0077;0.01127;0.01522;0.01945;0.02384;0.02823;0.03247;0.03638;0.03978;0.04248;0.04431;0.04484;0.04509;0.04504;0.04466;0.04397;0.04295;0.04161;0.03994;0.03795;0.03564;0.03305;0.03023;0.0272;0.02395;0.02039;0.01646;0.01214;0.00767;0.00349;0.0;-0.00349;-0.00767;-0.01214;-0.01646;-0.02039;-0.02395;-0.0272;-0.03023;-0.03305;-0.03564;-0.03795;-0.03994;-0.04161;-0.04295;-0.04397;-0.04466;-0.04504;-0.04509;-0.04484;-0.04431;-0.04248;-0.03978;-0.03638;-0.03247;-0.02823;-0.02384;-0.01945;-0.01522;-0.01127;-0.0077;-0.00463;-0.00218;-0.00057;0.0</z> | ||
</pointList> | ||
</wingAirfoil> | ||
</wingAirfoils> | ||
</profiles> | ||
</vehicles> | ||
</cpacs> |
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<?xml version="1.0" encoding="UTF-8"?> | ||
<cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" | ||
xsi:noNamespaceSchemaLocation="../schema/cpacs_schema.xsd" | ||
xsi:schemaLocation="http://www.cpacs.de/myTool ../schema/toolspecific_template.xsd"> | ||
<header> | ||
<name>Toolspecific example file</name> | ||
<creator>DLR</creator> | ||
<timestamp>2020-02-20T08:37:00</timestamp> | ||
<version>1.0</version> | ||
<cpacsVersion>3.2</cpacsVersion> | ||
</header> | ||
<toolspecific> | ||
<tool> | ||
<name>myToolName</name> | ||
<version>1.2.3</version> | ||
<myToolName xmlns="http://www.cpacs.de/myTool" schemaVersion="1.0"> | ||
<parentElement> | ||
<childElement1>stringValue</childElement1> | ||
<childElement2>1.0</childElement2> | ||
</parentElement> | ||
</myToolName> | ||
</tool> | ||
</toolspecific> | ||
</cpacs> |
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