}
Thrust = 0;
- ReverserAngle = 0.0;
Type = ttNozzle;
Area2 = (Diameter*Diameter/4.0)*M_PI;
AreaT = Area2/ExpR;
{
double pAtm = fdmex->GetAtmosphere()->GetPressure();
Thrust = max((double)0.0, (CfPc * AreaT + (PE - pAtm)*Area2) * nzlEff);
- vFn(1) = Thrust * cos(ReverserAngle);
+ vFn(1) = Thrust;
ThrustCoeff = max((double)0.0, CfPc / ((pAtm - PE) * Area2));
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-string FGNozzle::GetThrusterLabels(int id)
+string FGNozzle::GetThrusterLabels(int id, string delimeter)
{
std::ostringstream buf;
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-string FGNozzle::GetThrusterValues(int id)
+string FGNozzle::GetThrusterValues(int id, string delimeter)
{
std::ostringstream buf;