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IAgAvtrAdvFixedWingFourPointAero Interface

Description

Interface used to access the options for the FourPoint aerodynamic strategy in the advanced fixed wing tool.

Public Methods

Public Method ValidateDragDesignPointsValidate the drag design points - ensure the choices do not result in a singular system of equations.
Public Method ValidateLiftDesignPointsValidate the lift design points - ensure the choices do not result in a singular system of equations.

Public Properties

Public Property AOA_1Gets or sets the AOA for the first design point.
Public Property AOA_2Gets or sets the AOA for the second design point.
Public Property AOA_3Gets or sets the AOA for the third design point.
Public Property AOA_4Gets or sets the AOA for the fourth design point.
Public Property CD_1Gets or sets the drag coefficient for the first design point.
Public Property CD_2Gets or sets the drag coefficient for the second design point.
Public Property CD_3Gets or sets the drag coefficient for the third design point.
Public Property CD_4Gets or sets the drag coefficient for the fourth design point.
Public Property CL_1Gets or sets the lift coefficient for the first design point.
Public Property CL_2Gets or sets the lift coefficient for the second design point.
Public Property CL_3Gets or sets the lift coefficient for the third design point.
Public Property CL_4Gets or sets the lift coefficient for the fourth design point.
Public Property Mach_1Gets or sets the Mach for the first design point.
Public Property Mach_2Gets or sets the Mach for the second design point.
Public Property Mach_3Gets or sets the Mach for the third design point.
Public Property Mach_4Gets or sets the Mach for the fourth design point.
Public Property MaxAOAGets or sets the maximum AOA for the aircraft.

CoClasses that Implement IAgAvtrAdvFixedWingFourPointAero

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