Material functions

Functions
TiglReturnCode	tiglWingComponentSegmentGetMaterialCount (TiglCPACSConfigurationHandle cpacsHandle, const char *compSegmentUID, TiglStructureType structureType, double eta, double xsi, int *materialCount)
	Returns the number of materials defined at a point on the wing component segment surface. More...
TiglReturnCode	tiglWingComponentSegmentGetMaterialThickness (TiglCPACSConfigurationHandle cpacsHandle, const char *compSegmentUID, TiglStructureType structureType, double eta, double xsi, int materialIndex, double *thickness)
	Returns one of the material thicknesses of a given point on the wing component segment surface. The number of materials on that point has to be first queried using tiglWingComponentSegmentGetMaterialCount. More...
TiglReturnCode	tiglWingComponentSegmentGetMaterialUID (TiglCPACSConfigurationHandle cpacsHandle, const char *compSegmentUID, TiglStructureType structureType, double eta, double xsi, int materialIndex, char **uid)
	Returns one of the material UIDs of a given point on the wing component segment surface. The number of materials on that point has to be first queried using tiglWingComponentSegmentGetMaterialCount. More...

Detailed Description

Functions to query material information of wings/fuselages. Materials are currently ony implemented for the wing component segment. Here, materials for the lower and upper wing surface can be queried, which can be a material for the whole skin/surface or a material defined inside a wing cell. A wing cell material overwrites the global skin material, i.e. if the whole wing skin material is aluminum and the trailing edge is made of radar absorbing material, only the absorbing material is returned by the querying functions.

Function Documentation

TiglReturnCode tiglWingComponentSegmentGetMaterialCount	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	compSegmentUID,
		TiglStructureType	structureType,
		double	eta,
		double	xsi,
		int *	materialCount
	)

Returns the number of materials defined at a point on the wing component segment surface.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	compSegmentUID	UID of the component segment
[in]	structureType	Type of structure, where the materials are queried
[in]	eta	eta in the range 0.0 <= eta <= 1.0
[in]	xsi	xsi in the range 0.0 <= xsi <= 1.0
[out]	materialCount	Number of materials defined at the given coordinate

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_NULL_POINTER if compSegmentUID or materialCount is a null pointer
• TIGL_INDEX_ERROR if compSegmentUID or materialIndex is invalid
• TIGL_ERROR if some other error occurred

TiglReturnCode tiglWingComponentSegmentGetMaterialThickness	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	compSegmentUID,
		TiglStructureType	structureType,
		double	eta,
		double	xsi,
		int	materialIndex,
		double *	thickness
	)

Returns one of the material thicknesses of a given point on the wing component segment surface. The number of materials on that point has to be first queried using tiglWingComponentSegmentGetMaterialCount.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	compSegmentUID	UID of the component segment
[in]	structureType	Type of structure, where the materials are queried
[in]	eta	eta in the range 0.0 <= eta <= 1.0
[in]	xsi	xsi in the range 0.0 <= xsi <= 1.0
[in]	materialIndex	Index of the material to query (1 <= index <= materialCount)
[out]	thickness	Material thickness at the given coordinate. If no thickness is defined, thickness gets a negative value and TIGL_UNINITIALIZED is returned.

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_NULL_POINTER if compSegmentUID or thickness is a null pointer
• TIGL_INDEX_ERROR if compSegmentUID or materialIndex is invalid
• TIGL_UNINITIALIZED if no thickness is defined for the material
• TIGL_ERROR if some other error occurred

TiglReturnCode tiglWingComponentSegmentGetMaterialUID	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	compSegmentUID,
		TiglStructureType	structureType,
		double	eta,
		double	xsi,
		int	materialIndex,
		char **	uid
	)

Returns one of the material UIDs of a given point on the wing component segment surface. The number of materials on that point has to be first queried using tiglWingComponentSegmentGetMaterialCount.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	compSegmentUID	UID of the component segment
[in]	structureType	Type of structure, where the materials are queried
[in]	eta	eta in the range 0.0 <= eta <= 1.0
[in]	xsi	xsi in the range 0.0 <= xsi <= 1.0
[in]	materialIndex	Index of the material to query (1 <= index <= materialCount)
[out]	uid	Material uid at the given coordinate

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_NULL_POINTER if compSegmentUID is a null pointer
• TIGL_INDEX_ERROR if compSegmentUID or materialIndex is invalid
• TIGL_ERROR if some other error occurred