Beispiel #1
0
        public Vector3 GetAeroForce(Conditions conditions, float AoA, float pitchInput, out Vector3 torque, Vector3 torquePoint)
        {
            Vector3 aeroForce;
            Vector3 inflow = InflowVect(AoA);

            aeroForce = partCollection.GetAeroForce(inflow, conditions, AoA, pitchInput, out torque, torquePoint);

            float Q = 0.0005f * conditions.atmDensity * conditions.speed * conditions.speed;

            torque *= Q;
            return(aeroForce * Q);
        }