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02c29d0723
Separate screen are used to set the options for Selig and Bezier exports. There is no longer a need to set the value of m_AfExportType in the example script before exporting.
62 lines
2.2 KiB
Plaintext
62 lines
2.2 KiB
Plaintext
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void main()
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{
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Print( string( "Begin Airfoil Export Script\n" ) );
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Print( string( "--> Creating Wing Geometry\n" ) );
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//==== Add Wing Geometry ====//
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string wing_id = AddGeom( "WING" );
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//==== Turn Symmetry OFF ====//
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SetParmVal( FindParm( wing_id, "Sym_Planar_Flag", "Sym"), 0.0 ); // Note: bool input not supported in SetParmVal
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// Note: The shape of this wing was selected for demonstration purposes only
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//===== Add XSec ====//
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InsertXSec( wing_id, 1, XS_SIX_SERIES );
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//===== Change Some Parameters 1st Section ====//
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SetParmVal( wing_id, "Twist", "XSec_1", 20.0 );
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SetParmVal( wing_id, "InLEMode", "XSec_1", BLEND_MATCH_OUT_LE_TRAP );
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SetParmVal( wing_id, "InTEMode", "XSec_1", BLEND_MATCH_OUT_TE_TRAP );
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SetParmVal( wing_id, "ThickChord", "XSecCurve_0", 0.2 );
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//===== Define Number of Airfoils to Interpolate in Section 1 ====//
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SetParmVal( wing_id, "SectTess_U", "XSec_1", 9 );
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Update();
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//===== Change Some Parameters 2nd Section ====//
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SetParmVal( wing_id, "Span", "XSec_2", 3.0 );
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SetParmVal( wing_id, "Root_Chord", "XSec_2", 1.5 );
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SetParmVal( wing_id, "Tip_Chord", "XSec_2", 0.5 );
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SetParmVal( wing_id, "Sweep", "XSec_2", 50.0 );
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SetParmVal( wing_id, "Twist", "XSec_2", 20.0 );
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SetParmVal( wing_id, "Dihedral", "XSec_2", 20.0 );
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Update();
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//===== Set Airfoil Export Parms in Vehicle Parm Container ====//
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string veh_id = FindContainer( "Vehicle", 0 );
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SetParmVal( FindParm( veh_id, "AFWTessFactor", "AirfoilExport" ), 2.0 ); // double W tesselation for export
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SetParmVal( FindParm( veh_id, "AFAppendGeomIDFlag", "AirfoilExport" ), 1.0 ); // Note: bool input not supported in SetParmVal
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Update();
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//===== Export All Airfoils and Metadata *.csv ====//
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Print( string( "--> Exporting Airfoil Files\n" ) );
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ExportFile( "Airfoil_Metadata.csv", SET_ALL, EXPORT_SELIG_AIRFOIL );
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//==== Check For API Errors ====//
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while ( GetNumTotalErrors() > 0 )
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{
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ErrorObj err = PopLastError();
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Print( err.GetErrorString() );
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}
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Print( string( "COMPLETE\n" ) );
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} |