Describes polar aerodynamics of aircraft.
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#include <unicadoAcftXML.h>
Describes polar aerodynamics of aircraft.
◆ polarAerodynamics()
unicadoAcft::unicadoAerodynamics::polarAerodynamics::polarAerodynamics |
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◆ ~polarAerodynamics()
virtual unicadoAcft::unicadoAerodynamics::polarAerodynamics::~polarAerodynamics |
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◆ atmosphericModel
std::string unicadoAcft::unicadoAerodynamics::polarAerodynamics::atmosphericModel |
Name of atmospheric model
◆ deltaISA
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::deltaISA |
Temperature delta regarding ISA standard model [K]
◆ density
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::density |
◆ height
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::height |
◆ MMO
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::MMO |
Maximum operating Mach number [-]
◆ numberOfConfigurations
int unicadoAcft::unicadoAerodynamics::polarAerodynamics::numberOfConfigurations |
Number of aerodynamic configurations in polar file
◆ polarFile
std::string unicadoAcft::unicadoAerodynamics::polarAerodynamics::polarFile |
File name of aircraft polar
◆ Reynolds
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::Reynolds |
◆ SpeedOfSound
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::SpeedOfSound |
Air density [kg/m^3] Speed of sound [m/s]
◆ theAeroPolarPt
aerodynamics* unicadoAcft::unicadoAerodynamics::polarAerodynamics::theAeroPolarPt |
Pointer to aerodynamics data
◆ theConfigurations
std::vector<configuration> unicadoAcft::unicadoAerodynamics::polarAerodynamics::theConfigurations |
vector of class configuration objects
◆ velocity
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::velocity |
◆ Viscosity
double unicadoAcft::unicadoAerodynamics::polarAerodynamics::Viscosity |
Dynamic Viscosity [kg/(m*s)]
The documentation for this class was generated from the following files: