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API > API/Runtime > API/Runtime/ChaosVehiclesCore > API/Runtime/ChaosVehiclesCore/SimModule > API/Runtime/ChaosVehiclesCore/SimModule/FAerofoilSimModule
References
| Module | ChaosVehiclesCore |
| Header | /Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Public/SimModule/AerofoilModule.h |
| Include | #include "SimModule/AerofoilModule.h" |
| Source | /Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Private/SimModule/AerofoilModule.cpp |
float CalcDragCoefficient
(
float InAngleOfAttack,
float InControlSurfaceAngle
)
Remarks
Returns drag coefficient for the current angle of attack of the aerofoil surface