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SimpleFixedWingForwardFlightAerodynamicsComputeLiftCoefficient Method

Computes the lift coefficient from the provided parameters.

Namespace:  AGI.Foundation.AircraftPropagation
Assembly:  AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public static double ComputeLiftCoefficient(
	double liftCoefficientAtZeroAngleOfAttack,
	double liftCoefficientSlope,
	double angleOfAttack
)

Parameters

liftCoefficientAtZeroAngleOfAttack
Type: SystemDouble
The lift coefficient value at zero angle of attack.
liftCoefficientSlope
Type: SystemDouble
The lift coefficient slope with respect to the angle of attack in units of radians-1.
angleOfAttack
Type: SystemDouble
The angle of attack.

Return Value

Type: Double
The coefficient of lift.
See Also