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