FourPointAerodynamic#

class ansys.stk.core.stkobjects.aviator.FourPointAerodynamic#: Class defining the FourPoint aerodynamic strategy.

Overview#

Methods

`validate_lift_design_points`	Validate the lift design points - ensure the choices do not result in a singular system of equations.
`validate_drag_design_points`	Validate the drag design points - ensure the choices do not result in a singular system of equations.

Properties

`mach_1`	Get or set the Mach for the first design point.
`aoa_1`	Get or set the AOA for the first design point.
`cl_1`	Get or set the lift coefficient for the first design point.
`cd_1`	Get or set the drag coefficient for the first design point.
`mach_2`	Get or set the Mach for the second design point.
`aoa_2`	Get or set the AOA for the second design point.
`cl_2`	Get or set the lift coefficient for the second design point.
`cd_2`	Get or set the drag coefficient for the second design point.
`mach_3`	Get or set the Mach for the third design point.
`aoa_3`	Get or set the AOA for the third design point.
`cl_3`	Get or set the lift coefficient for the third design point.
`cd_3`	Get or set the drag coefficient for the third design point.
`mach_4`	Get or set the Mach for the fourth design point.
`aoa_4`	Get or set the AOA for the fourth design point.
`cl_4`	Get or set the lift coefficient for the fourth design point.
`cd_4`	Get or set the drag coefficient for the fourth design point.
`s_reference`	Get or set the aerodynamic reference area for the aircraft.
`max_aoa`	Get or set the maximum AOA for the aircraft.

Import detail#

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

Property detail#

property FourPointAerodynamic.mach_1: float#: Get or set the Mach for the first design point.

property FourPointAerodynamic.aoa_1: Any#: Get or set the AOA for the first design point.

property FourPointAerodynamic.cl_1: float#: Get or set the lift coefficient for the first design point.

property FourPointAerodynamic.cd_1: float#: Get or set the drag coefficient for the first design point.

property FourPointAerodynamic.mach_2: float#: Get or set the Mach for the second design point.

property FourPointAerodynamic.aoa_2: Any#: Get or set the AOA for the second design point.

property FourPointAerodynamic.cl_2: float#: Get or set the lift coefficient for the second design point.

property FourPointAerodynamic.cd_2: float#: Get or set the drag coefficient for the second design point.

property FourPointAerodynamic.mach_3: float#: Get or set the Mach for the third design point.

property FourPointAerodynamic.aoa_3: Any#: Get or set the AOA for the third design point.

property FourPointAerodynamic.cl_3: float#: Get or set the lift coefficient for the third design point.

property FourPointAerodynamic.cd_3: float#: Get or set the drag coefficient for the third design point.

property FourPointAerodynamic.mach_4: float#: Get or set the Mach for the fourth design point.

property FourPointAerodynamic.aoa_4: Any#: Get or set the AOA for the fourth design point.

property FourPointAerodynamic.cl_4: float#: Get or set the lift coefficient for the fourth design point.

property FourPointAerodynamic.cd_4: float#: Get or set the drag coefficient for the fourth design point.

property FourPointAerodynamic.s_reference: Any#: Get or set the aerodynamic reference area for the aircraft.

property FourPointAerodynamic.max_aoa: Any#: Get or set the maximum AOA for the aircraft.

Method detail#

FourPointAerodynamic.validate_lift_design_points(self, d_mach_1: float, d_aoa_1: Any, d_mach_2: float, d_aoa_2: Any, d_mach_3: float, d_aoa_3: Any, d_mach_4: float, d_aoa_4: Any) → bool#

Validate the lift design points - ensure the choices do not result in a singular system of equations.

Parameters:

d_mach_1 : float

d_aoa_1 : Any

d_mach_2 : float

d_aoa_2 : Any

d_mach_3 : float

d_aoa_3 : Any

d_mach_4 : float

d_aoa_4 : Any

Returns:

bool

FourPointAerodynamic.validate_drag_design_points(self, d_mach_1: float, d_c_l_1: float, d_mach_2: float, d_c_l_2: float, d_mach_3: float, d_c_l_3: float, d_mach_4: float, d_c_l_4: float) → bool#

Validate the drag design points - ensure the choices do not result in a singular system of equations.

Parameters:

d_mach_1 : float

d_c_l_1 : float

d_mach_2 : float

d_c_l_2 : float

d_mach_3 : float

d_c_l_3 : float

d_mach_4 : float

d_c_l_4 : float

Returns:

bool