Interface used to access the aerodynamics options for a rotorcraft.
![]() | Gets or sets the chord length of the blade. |
![]() | Gets or sets the drag coefficient when the rotor disc does not generate any lift. |
![]() | Gets or sets the induced drag coefficient, which accounts for how lift generation impacts drag. |
![]() | Gets or sets the number of blades on each rotor. |
![]() | Gets or sets the flat plate area for the fuselage. |
![]() | Gets or sets the slop factor that accounts for losses. |
![]() | Gets or sets the number of rotors. |
![]() | Gets or sets the diameter of the rotor. |
![]() | Gets or sets the Mach number of the advancing blade tip. |
![]() | Gets or sets the diameter of the tail rotor. |
![]() | Gets or sets the offset of the tail rotor. |