AdvancedFixedWingSubsonicAerodynamic#

class ansys.stk.core.stkobjects.aviator.AdvancedFixedWingSubsonicAerodynamic#

Class defining the subsonic aerodynamic strategy in the Advanced Fixed Wing Tool.

Overview#

geometry_type

Get or set the type of wing geometry for the aircraft.

geometry_mode_as_basic

Get the options for a basic geometry wing.

geometry_mode_as_variable

Get the options for a variable geometry wing.

max_aoa

Get or set the maximum angle of attack possible.

cd0

Get or set the parasitic drag coefficient of the aircraft when flying at a speed less than the Mach Divergence.

mach_divergence

Get or set the speed at which the aircraft begins to experience air compression.

transonic_mach_drag_factor

Get or set the factor applied to the aircraft’s parasitic drag coefficient when it is flying faster than the Mach Divergence.

Import detail#

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

Property detail#

property AdvancedFixedWingSubsonicAerodynamic.geometry_type: AdvancedFixedWingGeometry#

Get or set the type of wing geometry for the aircraft.

property AdvancedFixedWingSubsonicAerodynamic.geometry_mode_as_basic: AdvancedFixedWingGeometryBasic#

Get the options for a basic geometry wing.

property AdvancedFixedWingSubsonicAerodynamic.geometry_mode_as_variable: AdvancedFixedWingGeometryVariable#

Get the options for a variable geometry wing.

property AdvancedFixedWingSubsonicAerodynamic.max_aoa: Any#

Get or set the maximum angle of attack possible.

property AdvancedFixedWingSubsonicAerodynamic.cd0: float#

Get or set the parasitic drag coefficient of the aircraft when flying at a speed less than the Mach Divergence.

property AdvancedFixedWingSubsonicAerodynamic.mach_divergence: float#

Get or set the speed at which the aircraft begins to experience air compression.

property AdvancedFixedWingSubsonicAerodynamic.transonic_mach_drag_factor: float#

Get or set the factor applied to the aircraft’s parasitic drag coefficient when it is flying faster than the Mach Divergence.