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SimpleFixedWingForwardFlightAerodynamicsComputeDragCoefficient Method

Computes the drag 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 ComputeDragCoefficient(
	double dragCoefficientAtMinimum,
	double liftCoefficient,
	double oswaldEfficiencyFactor,
	double aspectRatio,
	double dragIndex
)

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.
See Also