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convertUNICADO2CPACS
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Class which contains the aerodynamic performance data. More...
#include <cpacsAcftXML.h>
Public Member Functions | |
cpacsAeroPerformanceMap () | |
Constructor of class cpacsAeroPerformanceMap. More... | |
virtual | ~cpacsAeroPerformanceMap () |
Destructor of class cpacsAeroPerformanceMap. More... | |
Public Attributes | |
information | info |
std::string | theAtmosphericModel |
std::string | theDeltaTemperature |
std::string | theMach |
std::string | theReynolds |
std::string | theAltitude |
std::string | theYawAngle |
std::string | theAlpha |
std::string | thecd |
std::string | thecl |
std::string | thecm |
Class which contains the aerodynamic performance data.
cpacsAcft::cpacsAeroPerformanceMap::cpacsAeroPerformanceMap | ( | ) |
Constructor of class cpacsAeroPerformanceMap.
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virtual |
Destructor of class cpacsAeroPerformanceMap.
information cpacsAcft::cpacsAeroPerformanceMap::info |
Object of the information class that provides the CPACS aero performance map infos like uID and description
std::string cpacsAcft::cpacsAeroPerformanceMap::theAlpha |
Angle of attack [deg]
std::string cpacsAcft::cpacsAeroPerformanceMap::theAltitude |
Altitude [m]
std::string cpacsAcft::cpacsAeroPerformanceMap::theAtmosphericModel |
Atmospheric model (e.g. "ISA" for ICAO Standard atmosphere)
std::string cpacsAcft::cpacsAeroPerformanceMap::thecd |
Drag coefficient
std::string cpacsAcft::cpacsAeroPerformanceMap::thecl |
Lift coefficient
std::string cpacsAcft::cpacsAeroPerformanceMap::thecm |
Moment coefficient
std::string cpacsAcft::cpacsAeroPerformanceMap::theDeltaTemperature |
Offset from temperature of the atmospheric model [K]
std::string cpacsAcft::cpacsAeroPerformanceMap::theMach |
Mach number
std::string cpacsAcft::cpacsAeroPerformanceMap::theReynolds |
Reynolds number
std::string cpacsAcft::cpacsAeroPerformanceMap::theYawAngle |
Yaw angle [deg]