AdvancedFixedWingSubSuperHypersonicAerodynamic#

class ansys.stk.core.stkobjects.aviator.AdvancedFixedWingSubSuperHypersonicAerodynamic#: Class defining the Sub/Super/Hypersonic aerodynamic strategy in the Advanced Fixed Wing Tool.

Overview#

Properties

`max_aoa`	Get or set the maximum angle of attack possible.
`transonic_min_mach`	Get or set the minimum speed at which the aircraft begins to experience air compression.
`transonic_max_mach`	Get or set the maximum speed, below supersonic, at which the aircraft begins to experience air compression.
`super_hyper_mach_transition`	Get or set the minimum speed at which the air flow will be treated as hypersonic.
`leading_edge_frontal_area_ratio`	Get or set the frontal face thickness of the aircraft’s wings at their leading edge.
`subsonic_aspect_ratio`	Get or set the aircraft’s wingspan squared divided by the wing area.
`transonic_mach_drag_factor`	Get or set 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.
`wave_drag_factor`	Get or set the scalar value that models drag produced by shock waves at or near the aircraft’s critical Mach number.

from ansys.stk.core.stkobjects.aviator import AdvancedFixedWingSubSuperHypersonicAerodynamic

property AdvancedFixedWingSubSuperHypersonicAerodynamic.max_aoa: Any#: Get or set the maximum angle of attack possible.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.transonic_min_mach: float#: Get or set the minimum speed at which the aircraft begins to experience air compression.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.transonic_max_mach: float#: Get or set the maximum speed, below supersonic, at which the aircraft begins to experience air compression.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.super_hyper_mach_transition: float#: Get or set the minimum speed at which the air flow will be treated as hypersonic.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.leading_edge_frontal_area_ratio: float#: Get or set the frontal face thickness of the aircraft’s wings at their leading edge.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.subsonic_aspect_ratio: float#: Get or set the aircraft’s wingspan squared divided by the wing area.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.transonic_mach_drag_factor: float#: Get or set 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.

property AdvancedFixedWingSubSuperHypersonicAerodynamic.wave_drag_factor: float#: Get or set the scalar value that models drag produced by shock waves at or near the aircraft’s critical Mach number.