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convertUNICADO2CPACS
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Class which describes the airfoil definition of a control surface between inner and outer border. More...
#include <cpacsAcftXML.h>
Public Member Functions | |
intermediateAirfoil () | |
Constructor of class intermediateAirfoil. More... | |
virtual | ~intermediateAirfoil () |
Destructor of class intermediateAirfoil. More... | |
Public Attributes | |
double | eta |
std::string | airfoilUID |
double | rotX |
double | rotZ |
double | scalY |
double | scalZ |
Class which describes the airfoil definition of a control surface between inner and outer border.
cpacsAcft::controlSurface::intermediateAirfoil::intermediateAirfoil | ( | ) |
Constructor of class intermediateAirfoil.
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virtual |
Destructor of class intermediateAirfoil.
std::string cpacsAcft::controlSurface::intermediateAirfoil::airfoilUID |
Reference to the CPACS airfoil uID.
double cpacsAcft::controlSurface::intermediateAirfoil::eta |
Relative spanwise coordinate (eta) of the control surface, where the leading edge of the airfoil is placed.
double cpacsAcft::controlSurface::intermediateAirfoil::rotX |
Rotation around axis from leading edge point to trailing edge point of the control surface [deg]
double cpacsAcft::controlSurface::intermediateAirfoil::rotZ |
Rotation of the airfoil around the control surface middle plane normal direction. [deg]
double cpacsAcft::controlSurface::intermediateAirfoil::scalY |
Scaling of the airfoil in spanwise direction (not used for 2D airfoils).
double cpacsAcft::controlSurface::intermediateAirfoil::scalZ |
Scaling in thickness direction of the airfoil.