AircraftBasicFixedWingAerodynamic#

class ansys.stk.core.stkobjects.aviator.AircraftBasicFixedWingAerodynamic#: Class defining the basic fixed wing aerodynamic options for a basic acceleration performance model of an Aviator aircraft.

Overview#

Properties

`forward_flight_reference_area`	Get or set the area of the lifting surface of the aircraft.
`forward_flight_use_compressible_flow`	Opt to define the aerodynamic parameters for forward flight with respect to supersonic flight conditions.
`forward_flight_cl0`	Get or set the coefficient of lift at zero angle of attack.
`forward_flight_cl_alpha`	Get or set the slope of the coefficient of lift curve.
`forward_flight_min_aoa`	Get or set the minimum angle of attack possible.
`forward_flight_max_aoa`	Get or set the maximum angle of attack possible.
`forward_flight_cd0`	Get or set the coefficient of drag of the lifting surface at zero angle of attack.
`forward_flight_k`	Get or set the coefficient of induced drag.
`takeoff_landing_reference_area`	Get or set the area of the lifting surface of the aircraft.
`takeoff_landing_use_compressible_flow`	Opt to define the aerodynamic parameters for takeoff and landing with respect to supersonic flight conditions.
`takeoff_landing_cl0`	Get or set the coefficient of lift at zero angle of attack.
`takeoff_landing_cl_alpha`	Get or set the slope of the coefficient of lift curve.
`takeoff_landing_min_aoa`	Get or set the minimum angle of attack possible.
`takeoff_landing_max_aoa`	Get or set the maximum angle of attack possible.
`takeoff_landing_cd0`	Get or set the coefficient of drag of the lifting surface at zero angle of attack.
`takeoff_landing_k`	Get or set the coefficient of induced drag.

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

property AircraftBasicFixedWingAerodynamic.forward_flight_reference_area: float#: Get or set the area of the lifting surface of the aircraft.

property AircraftBasicFixedWingAerodynamic.forward_flight_use_compressible_flow: bool#: Opt to define the aerodynamic parameters for forward flight with respect to supersonic flight conditions.

property AircraftBasicFixedWingAerodynamic.forward_flight_cl0: float#: Get or set the coefficient of lift at zero angle of attack.

property AircraftBasicFixedWingAerodynamic.forward_flight_cl_alpha: float#: Get or set the slope of the coefficient of lift curve.

property AircraftBasicFixedWingAerodynamic.forward_flight_min_aoa: Any#: Get or set the minimum angle of attack possible.

property AircraftBasicFixedWingAerodynamic.forward_flight_max_aoa: Any#: Get or set the maximum angle of attack possible.

property AircraftBasicFixedWingAerodynamic.forward_flight_cd0: float#: Get or set the coefficient of drag of the lifting surface at zero angle of attack.

property AircraftBasicFixedWingAerodynamic.forward_flight_k: float#: Get or set the coefficient of induced drag.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_reference_area: float#: Get or set the area of the lifting surface of the aircraft.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_use_compressible_flow: bool#: Opt to define the aerodynamic parameters for takeoff and landing with respect to supersonic flight conditions.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_cl0: float#: Get or set the coefficient of lift at zero angle of attack.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_cl_alpha: float#: Get or set the slope of the coefficient of lift curve.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_min_aoa: Any#: Get or set the minimum angle of attack possible.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_max_aoa: Any#: Get or set the maximum angle of attack possible.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_cd0: float#: Get or set the coefficient of drag of the lifting surface at zero angle of attack.

property AircraftBasicFixedWingAerodynamic.takeoff_landing_k: float#: Get or set the coefficient of induced drag.