Describes the lift coefficients of aircraft.
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#include <unicadoAcftXML.h>
Describes the lift coefficients of aircraft.
◆ liftCoefficients()
unicadoAcft::unicadoAerodynamics::liftCoefficients::liftCoefficients |
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◆ ~liftCoefficients()
virtual unicadoAcft::unicadoAerodynamics::liftCoefficients::~liftCoefficients |
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◆ cl_opt_stab
double unicadoAcft::unicadoAerodynamics::liftCoefficients::cl_opt_stab |
Lift coefficient at best loverD, stabalizer proportion [-]
◆ cl_opt_wing
double unicadoAcft::unicadoAerodynamics::liftCoefficients::cl_opt_wing |
Lift coefficient at best loverD, wing proportion [-]
◆ clDesign
double unicadoAcft::unicadoAerodynamics::liftCoefficients::clDesign |
Design lift coefficient [-]
◆ clMaxLanding
double unicadoAcft::unicadoAerodynamics::liftCoefficients::clMaxLanding |
Maximum lift coefficient landing configuration [-]
◆ clMaxTo
double unicadoAcft::unicadoAerodynamics::liftCoefficients::clMaxTo |
Maximum lift coefficient take-of configuration [-]
◆ clOptimumCruise
double unicadoAcft::unicadoAerodynamics::liftCoefficients::clOptimumCruise |
Lift coefficient at best loverD [-]
The documentation for this class was generated from the following file: