FAerofoil::CalcDynamicPressure

Dynamic air pressure = 0.5 * AirDensity * Vsqr This function reduces the dynamic pressure in a linear fashion with altitude between MinCeiling & MaxCeiling in order to limit the aircrafts altitude with a 'natural feel' without having a hard limit

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References

Module	ChaosVehiclesCore
Header	/Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Public/AerofoilSystem.h
Include	#include "AerofoilSystem.h"
Source	/Engine/Source/Runtime/Experimental/ChaosVehicles/ChaosVehiclesCore/Private/AerofoilSystem.cpp

Syntax

float CalcDynamicPressure
(
float VelocitySqr,
float InAltitude
)

Remarks

Dynamic air pressure = 0.5 * AirDensity * Vsqr This function reduces the dynamic pressure in a linear fashion with altitude between MinCeiling & MaxCeiling in order to limit the aircrafts altitude with a 'natural feel' without having a hard limit