Get point and tangent depending on the parameter on a fuselage guide curves. More...
#include "tigl_internal.h"
#include "TopoDS_Wire.hxx"
#include "TopoDS_Edge.hxx"
#include "TopTools_SequenceOfShape.hxx"
#include "gp_Pnt.hxx"
#include "gp_Vec.hxx"
#include "CCPACSGuideCurve.h"
Data Structures | |
class | tigl::CCPACSWingProfileGetPointAlgo |
Namespaces | |
tigl | |
The CTiglShapeCache class acts as a storage for all kinds of intermediate shape results in order to improve speed of reoccurent calculations. | |
Get point and tangent depending on the parameter on a fuselage guide curves.
This class takes the concatenated lower and upper wing profile wire (in this order) and provides the point and the tangent for a given parameter alpha along the curve. The curve starts at the trailing edge (alpha=-1), runs through the upper fuselage profile towards the leading edge (alpha=0) and returns to the trailing edge (alpha=1) via the lower fuselage profile