Functions for volume calculations

Functions
TiglReturnCode	tiglFuselageGetSegmentVolume (TiglCPACSConfigurationHandle cpacsHandle, int fuselageIndex, int segmentIndex, double *volumePtr)
	Returns the volume of a segment of a fuselage. More...
TiglReturnCode	tiglFuselageGetVolume (TiglCPACSConfigurationHandle cpacsHandle, int fuselageIndex, double *volumePtr)
	Returns the volume of the fuselage. More...
TiglReturnCode	tiglWingGetSegmentVolume (TiglCPACSConfigurationHandle cpacsHandle, int wingIndex, int segmentIndex, double *volumePtr)
	Returns the volume of a segment of a wing. More...
TiglReturnCode	tiglWingGetVolume (TiglCPACSConfigurationHandle cpacsHandle, int wingIndex, double *volumePtr)
	Returns the volume of the wing. More...

Detailed Description

Function for volume calculations on wings/fuselages.

Function Documentation

tiglFuselageGetSegmentVolume()

TiglReturnCode tiglFuselageGetSegmentVolume	(	TiglCPACSConfigurationHandle	cpacsHandle,
		int	fuselageIndex,
		int	segmentIndex,
		double *	volumePtr
	)

Returns the volume of a segment of a fuselage.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	fuselageIndex	The index of a fuselage, starting at 1
[in]	segmentIndex	The index of a segment, starting at 1
[out]	volumePtr	The pointer to a variable for the volume of the fuselage

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_INDEX_ERROR if fuselageIndex, sectionIndex or elementIndex are not valid
• TIGL_NULL_POINTER if volumePtr is a null pointer
• TIGL_ERROR if some other error occurred

tiglFuselageGetVolume()

TiglReturnCode tiglFuselageGetVolume	(	TiglCPACSConfigurationHandle	cpacsHandle,
		int	fuselageIndex,
		double *	volumePtr
	)

Returns the volume of the fuselage.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	fuselageIndex	Index of the fuselage to calculate the volume, starting at 1
[out]	volumePtr	The volume of the fuselage

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_INDEX_ERROR if fuselageIndex is less or equal zero
• TIGL_ERROR if some other error occurred

tiglWingGetSegmentVolume()

TiglReturnCode tiglWingGetSegmentVolume	(	TiglCPACSConfigurationHandle	cpacsHandle,
		int	wingIndex,
		int	segmentIndex,
		double *	volumePtr
	)

Returns the volume of a segment of a wing.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	wingIndex	The index of a wing, starting at 1
[in]	segmentIndex	The index of a segment, starting at 1
[out]	volumePtr	The pointer to a variable for the volume of the wing

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_INDEX_ERROR if wingIndex, sectionIndex or elementIndex are not valid
• TIGL_NULL_POINTER if volumePtr is a null pointer
• TIGL_ERROR if some other error occurred

tiglWingGetVolume()

TiglReturnCode tiglWingGetVolume	(	TiglCPACSConfigurationHandle	cpacsHandle,
		int	wingIndex,
		double *	volumePtr
	)

Returns the volume of the wing.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	wingIndex	Index of the Wing to calculate the volume, starting at 1
[out]	volumePtr	The volume of the wing

Returns

• TIGL_SUCCESS if no error occurred
• TIGL_NOT_FOUND if no configuration was found for the given handle
• TIGL_INDEX_ERROR if wingIndex is less or equal zero
• TIGL_ERROR if some other error occurred