private void SetStaticSimulation()
{
ambientTherm = EngineThermodynamics.StandardConditions(true);
inletTherm = ambientTherm;
inletTherm.P *= AJEInlet.OverallStaticTPR(defaultTPR);
areaRatio = 1d;
lastPropellantFraction = 1d;
}
protected void PushAreaToInlet()
{
if (intakeMatchArea)
{
AJEInlet intake = part.FindModuleImplementing <AJEInlet>();
if (intake != null)
{
intake.Area = RequiredIntakeArea();
}
}
}
public void FitEngine(double dryThrust, double drySFC, double wetThrust, double idleNozzlePressureRatio, double defaultTPR = 1d)
{
float TPR = AJEInlet.OverallStaticTPR((float)defaultTPR);
SetEngineState(true, 1d);
SetStaticConditions(usePlanetarium: false, overallTPR: TPR);
double dryThrottle = Afterburning ? 2d / 3d : 1d;
this.drySFC = drySFC;
if (drySFC > 0d)
{
CalculatePerformance(1d, dryThrottle, 1d, 1d);
if (Math.Abs(SFC / drySFC - 1d) > 0.0001d)
{
h_f = SolverMathUtil.BrentsMethod(DrySFCFittingFunction, 10e6, 200e6, maxIter: 1000);
CalculateTTR();
}
}
// Min throttle
// Set to make sure tailpipe pressure is greater than ambient
minThrottle = 0.01f;
CalculatePerformance(1d, 0f, 1d, 1d);
idleNPR = idleNozzlePressureRatio;
if (th7.P > 1.25 * th0.P)
{
minThrottle = 0.01f;
}
else
{
CalculatePerformance(1d, dryThrottle, 1d, 1d);
if (th7.P < idleNPR * th0.P)
{
Debug.Log("Cannot fit min throttle because jet pipe pressure is too low. Perhaps TIT is too low or CPR is too high.");
minThrottle = 0.01f;
}
else
{
minThrottle = SolverMathUtil.BrentsMethod(MinThrottleFittingFunction, 0.01f, 1f, maxIter: 1000);
}
}
CalculatePerformance(1d, dryThrottle, 1d, 1d);
double aTurbine = th4.CalculateFlowArea(coreAirflow * th4.MassRatio, 1d);
double fakeAref = th1.CalculateFlowArea(coreAirflow, 0.5d);
turbineAreaRatio = aTurbine / fakeAref;
this.dryThrust = dryThrust;
if (dryThrust > 0d)
{
CalculatePerformance(1d, dryThrottle, 1d, 1d);
Aref *= dryThrust / thrust;
}
this.wetThrust = wetThrust;
if (wetThrust > 0d)
{
bool doFit = true;
double oldTt7 = Tt7;
if (Tt7 <= 0d)
{
Tt7 = 2500d;
}
else
{
CalculatePerformance(1d, 1d, 1d, 1d);
if (Math.Abs(thrust / wetThrust - 1d) <= 0.0001d)
{
// TAB already correct, no need to fit
doFit = false;
}
}
// Check bounds
if (doFit)
{
CalculatePerformance(1d, 2d / 3d, 1d, 1d);
if (thrust >= wetThrust)
{
Debug.LogWarning("Cannot fit wet thrust on engine because dry thrust is already greater than specified value.");
doFit = false;
}
Tt7 = 4000d;
CalculatePerformance(1d, 1d, 1d, 1d);
if (thrust <= wetThrust)
{
Debug.LogWarning("Cannot fit wet thrust on engine solver because it would require an afterburner temperature of more than 4000 K.");
doFit = false;
}
}
if (doFit)
{
Tt7 = SolverMathUtil.BrentsMethod(WetThrustFittingFunction, th5.T, 4000d, maxIter: 1000);
}
else
{
Tt7 = oldTt7;
}
}
}