Description
Interface used to access Basic Fixed Wing Aerodynamics interface for the Basic Acceleration Model of an aircraft.
Public Properties
 ForwardFlightCd0 | The coefficient of drag of the lifting surface at zero angle of attack. |
| ForwardFlightCl0 | The coefficient of lift at zero angle of attack. |
| ForwardFlightClAlpha | The slope of the coefficient of lift curve. |
| ForwardFlightK | The coefficient of induced drag. |
| ForwardFlightMaxAOA | The maximum angle of attack possible. |
| ForwardFlightMinAOA | The minimum angle of attack possible. |
| ForwardFlightReferenceArea | The area of the lifting surface of the aircraft. |
| ForwardFlightUseCompressibleFlow | Opt to define the aerodynamic parameters for forward flight with respect to supersonic flight conditions. |
| TakeoffLandingCd0 | The coefficient of drag of the lifting surface at zero angle of attack. |
| TakeoffLandingCl0 | The coefficient of lift at zero angle of attack. |
| TakeoffLandingClAlpha | The slope of the coefficient of lift curve. |
| TakeoffLandingK | The coefficient of induced drag. |
| TakeoffLandingMaxAOA | The maximum angle of attack possible. |
| TakeoffLandingMinAOA | The minimum angle of attack possible. |
| TakeoffLandingReferenceArea | The area of the lifting surface of the aircraft. |
| TakeoffLandingUseCompressibleFlow | Opt to define the aerodynamic parameters for takeoff and landing with respect to supersonic flight conditions. |