SimpleFixedWingForwardFlightAerodynamicsComputeDragCoefficient Method

Computes the drag coefficient from the provided parameters.

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public static double ComputeDragCoefficient(
	double dragCoefficientAtMinimum,
	double liftCoefficient,
	double oswaldEfficiencyFactor,
	double aspectRatio,
	double dragIndex
)

Public Shared Function ComputeDragCoefficient ( 
	dragCoefficientAtMinimum As Double,
	liftCoefficient As Double,
	oswaldEfficiencyFactor As Double,
	aspectRatio As Double,
	dragIndex As Double
) As Double

public:
static double ComputeDragCoefficient(
	double dragCoefficientAtMinimum, 
	double liftCoefficient, 
	double oswaldEfficiencyFactor, 
	double aspectRatio, 
	double dragIndex
)

static member ComputeDragCoefficient : 
        dragCoefficientAtMinimum : float * 
        liftCoefficient : float * 
        oswaldEfficiencyFactor : float * 
        aspectRatio : float * 
        dragIndex : float -> float

Parameters

dragCoefficientAtMinimum: Type: SystemDouble
The minimum drag coefficient value.
liftCoefficient: Type: SystemDouble
The coefficient of lift.
oswaldEfficiencyFactor: Type: SystemDouble
The Oswald efficiency factor for the wing.
aspectRatio: Type: SystemDouble
The aspect ratio of the wing.
dragIndex: Type: SystemDouble
The drag index.

Return Value

Type: Double
The coefficient of drag.

Reference

SimpleFixedWingForwardFlightAerodynamics Class

AGI.Foundation.AircraftPropagation Namespace

SimpleFixedWingForwardFlightAerodynamicsAddLanguageSpecificTextSet("LSTF11C15E1_0?cpp=::|nu=.");ComputeDragCoefficient Method

Parameters

Return Value

Reference

SimpleFixedWingForwardFlightAerodynamicsComputeDragCoefficient Method