C# (CSharp) AircraftParameters.GetLiftCoefficient 예제들

예제 #1

 /// <summary>
 /// Calculates the lift force.
 /// </summary>
 /// <returns></returns>
 private double GetLiftForce()
 {
     // F = (1/2)*Cl*V^2*S
     return(AircraftParameters.GetLiftCoefficient(Alpha) * (Vx * Vx + Vz * Vz) * rhoSurface);
 }