Interface used to access the options for the supersonic aerodynamic strategy in the advanced fixed wing tool.
![]() | Get the options for a basic geometry wing. |
![]() | Get the options for a variable geometry wing. |
![]() | Gets or sets the type of wing geometry for the aircraft. |
![]() | Gets or sets the ability of the wing's leading edge to ingest turbulent airflow and thereby reduce induced drag. |
![]() | Gets or sets the maximum angle of attack possible. |
![]() | Gets or sets the parasitic drag coefficient of the aircraft when flying at a speed less than the Mach Divergence. |
![]() | Gets or sets the scalar value applied to the aircraft's parasitic drag coefficient when it is flying faster than the Supersonic Max Mach. |
![]() | Gets or sets the speed at which the Supersonic Mach Drag Factor is applied. |
![]() | Gets or sets the factor applied to the aircraft's parasitic drag coefficient when it is flying between the Transonic Min Mach and Transonic Mach Drag Factor speeds. |
![]() | Gets or sets the maximum speed, below supersonic, at which the aircraft begins to experience air compression. |
![]() | Gets or sets the minimum speed at which the aircraft begins to experience air compression. |