Functions
TIGL_COMMON_EXPORT TiglReturnCode	tiglCheckPointInside (TiglCPACSConfigurationHandle cpacsHandle, double px, double py, double pz, const char componentUID, TiglBoolean isInside)
	Checks whether a point lies inside the given geometric object. More...

TIGL_COMMON_EXPORT TiglReturnCode	tiglComponentGetHashCode (TiglCPACSConfigurationHandle cpacsHandle, const char componentUID, int hashCodePtr)
	Returns a unique HashCode for a geometric component. More...

TIGL_COMMON_EXPORT TiglReturnCode	tiglConfigurationGetLength (TiglCPACSConfigurationHandle cpacsHandle, double *pLength)
	Returns the length of the plane. More...

TIGL_COMMON_EXPORT const char *	tiglGetErrorString (TiglReturnCode errorCode)
	Translates an error code into a string. More...

TIGL_COMMON_EXPORT TiglReturnCode	tiglWingGetMAC (TiglCPACSConfigurationHandle cpacsHandle, const char wingUID, double mac_chord, double mac_x, double mac_y, double *mac_z)
	This function calculates location of the quarter of mean aerodynamic chord, and gives the chord lenght as well. More...

TIGL_COMMON_EXPORT TiglReturnCode	tiglWingGetSpan (TiglCPACSConfigurationHandle cpacsHandle, const char wingUID, double pSpan)
	Returns the span of a wing. More...

Detailed Description

Generic utility functions for geometric components that fits not only to wings or fuselages.

Function Documentation

TIGL_COMMON_EXPORT TiglReturnCode tiglCheckPointInside	(	TiglCPACSConfigurationHandle	cpacsHandle,
		double	px,
		double	py,
		double	pz,
		const char *	componentUID,
		TiglBoolean *	isInside
	)

Checks whether a point lies inside the given geometric object.

This function works only for solid objects!

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	px	X coordinate of point
[in]	py	Y coordinate of point
[in]	pz	Z coordinate of point
[in]	componentUID	UID of the component (e.g. a fuselage UID, wing UID, wing segment UID ...)
[out]	isInside	Returns, whether the point lies inside the object or not.

Returns

TIGL_SUCCESS if no error occurred.
TIGL_NOT_FOUND if no configuration was found for the given handle.
TIGL_UID_ERROR if the component does not exist or is not a geometric object.
TIGL_NULL_POINTER if componentUID or isInside are null.
TIGL_ERROR if some error occurred, e.g. the component is not a solid object.

TIGL_COMMON_EXPORT TiglReturnCode tiglComponentGetHashCode	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	componentUID,
		int *	hashCodePtr
	)

Returns a unique HashCode for a geometric component.

The component, for example a wing or a fuselage, could be specified via its UID. The HashCode is the same as long as the geometry of this component has not changed. The HashCode is valid through the current session only! The hash value is computed from the value of the underlying shape reference.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	componentUID	The uid of the component for which the hash should be computed
[out]	hashCodePtr	The pointer to a hash value to represent this shape

Returns

TIGL_SUCCESS if no error occurred
TIGL_NOT_FOUND if no configuration was found for the given handle
TIGL_NULL_POINTER if surfaceAreaPtr is a null pointer
TIGL_ERROR if some other error occurred

TIGL_COMMON_EXPORT TiglReturnCode tiglConfigurationGetLength	(	TiglCPACSConfigurationHandle	cpacsHandle,
		double *	pLength
	)

Returns the length of the plane.

The calculation of the airplane lenght is realized as follows:

All part of the configuration (currently all wing and fuselage segments) are put into a bounding box. The length of the plane is returned as the length of the box in x-direction.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[out]	pLength	Length of plane

Returns: Error code

TIGL_COMMON_EXPORT const char* tiglGetErrorString ( TiglReturnCode errorCode )

Translates an error code into a string.

Parameters

[in] errorCode Return value of a tigl function

Returns: Error code as a string.

TIGL_COMMON_EXPORT TiglReturnCode tiglWingGetMAC	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	wingUID,
		double *	mac_chord,
		double *	mac_x,
		double *	mac_y,
		double *	mac_z
	)

This function calculates location of the quarter of mean aerodynamic chord, and gives the chord lenght as well.

It uses the classical method that can be applied to trapozaidal wings. This method is used for each segment. The values are found by taking into account of sweep and dihedral. But the effect of insidance angle is neglected. These values should coinside with the values found with tornado tool.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	wingUID	UID of the Wing
[out]	mac_chord	Mean areadynamic chord length
[out]	mac_x,mac_y,mac_z	- Position of the MAC

Returns

TIGL_SUCCESS if no error occurred
TIGL_NULL_POINTER if wingUID, mac_chord, mac_x, mac_y or mac_z are null pointers
TIGL_ERROR In case of an unknown error

TIGL_COMMON_EXPORT TiglReturnCode tiglWingGetSpan	(	TiglCPACSConfigurationHandle	cpacsHandle,
		const char *	wingUID,
		double *	pSpan
	)

Returns the span of a wing.

The calculation of the wing span is realized as follows:

If the wing is mirrored at a symmetry plane (like the main wing), the wing body and its mirrored counterpart are computed and are put into a bounding box. The length of the box in a specific space dimension is returned as the wing span depending on the symmetry plane (y direction for x-z planes, z direction for x-y planes, x direction for y-z symmetry planes).
If no symmetry plane is defined (e.g. for the fins), the largest dimension of the bounding box around the wing is returned.

Parameters

[in]	cpacsHandle	Handle for the CPACS configuration
[in]	wingUID	UID of the Wing
[out]	pSpan	Wing span

Returns: Error code

Functions

Detailed Description

Function Documentation