Description
Interface used to access Basic Fixed Wing Aerodynamics interface for the Basic Acceleration Model of an aircraft.
Public Properties
 ForwardFlightCd0 | Gets or sets the coefficient of drag of the lifting surface at zero angle of attack. |
| ForwardFlightCl0 | Gets or sets the coefficient of lift at zero angle of attack. |
| ForwardFlightClAlpha | Gets or sets the slope of the coefficient of lift curve. |
| ForwardFlightK | Gets or sets the coefficient of induced drag. |
| ForwardFlightMaxAOA | Gets or sets the maximum angle of attack possible. |
| ForwardFlightMinAOA | Gets or sets the minimum angle of attack possible. |
| ForwardFlightReferenceArea | Gets or sets 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 | Gets or sets the coefficient of drag of the lifting surface at zero angle of attack. |
| TakeoffLandingCl0 | Gets or sets the coefficient of lift at zero angle of attack. |
| TakeoffLandingClAlpha | Gets or sets the slope of the coefficient of lift curve. |
| TakeoffLandingK | Gets or sets the coefficient of induced drag. |
| TakeoffLandingMaxAOA | Gets or sets the maximum angle of attack possible. |
| TakeoffLandingMinAOA | Gets or sets the minimum angle of attack possible. |
| TakeoffLandingReferenceArea | Gets or sets 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. |