SimpleFixedWingForwardFlightAerodynamicsComputeLiftCoefficient Method

Computes the lift coefficient from the provided parameters.

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public static double ComputeLiftCoefficient(
	double liftCoefficientAtZeroAngleOfAttack,
	double liftCoefficientSlope,
	double angleOfAttack
)

Public Shared Function ComputeLiftCoefficient ( 
	liftCoefficientAtZeroAngleOfAttack As Double,
	liftCoefficientSlope As Double,
	angleOfAttack As Double
) As Double

public:
static double ComputeLiftCoefficient(
	double liftCoefficientAtZeroAngleOfAttack, 
	double liftCoefficientSlope, 
	double angleOfAttack
)

static member ComputeLiftCoefficient : 
        liftCoefficientAtZeroAngleOfAttack : float * 
        liftCoefficientSlope : float * 
        angleOfAttack : float -> float

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.

Reference

SimpleFixedWingForwardFlightAerodynamics Class

AGI.Foundation.AircraftPropagation Namespace

SimpleFixedWingForwardFlightAerodynamicsAddLanguageSpecificTextSet("LST89B312DC_0?cpp=::|nu=.");ComputeLiftCoefficient Method

Parameters

Return Value

Reference

SimpleFixedWingForwardFlightAerodynamicsComputeLiftCoefficient Method