FGSimTurbine::FGSimTurbine(FGFDMExec* exec, FGConfigFile* cfg) : FGEngine(exec)
{
SetDefaults();
- FGEngine::Type=etSimTurbine;
+
Load(cfg);
Debug(0);
}
phase = tpRun;
N2 = IdleN2;
N1 = IdleN1;
- OilTemp_degK = TAT + 10;
+ OilTemp_degK = 366.0;
Cutoff = false;
}
else {
double FGSimTurbine::Off(void)
{
- double qbar = Translation->Getqbar();
- Running = false;
- FuelFlow_pph = 0.0;
- N1 = Seek(&N1, qbar/10.0, N1/2.0, N1/2.0);
- N2 = Seek(&N2, qbar/15.0, N2/2.0, N2/2.0);
- EGT_degC = Seek(&EGT_degC, TAT, 11.7, 7.3);
- OilTemp_degK = Seek(&OilTemp_degK, TAT + 273.0, 0.2, 0.2);
- OilPressure_psi = N2 * 0.62;
- EPR = 1.0;
- return 0.0;
+ double qbar = Translation->Getqbar();
+ Running = false;
+ FuelFlow_pph = Seek(&FuelFlow_pph, 0, 1000.0, 10000.0);
+ N1 = Seek(&N1, qbar/10.0, N1/2.0, N1/2.0);
+ N2 = Seek(&N2, qbar/15.0, N2/2.0, N2/2.0);
+ EGT_degC = Seek(&EGT_degC, TAT, 11.7, 7.3);
+ OilTemp_degK = Seek(&OilTemp_degK, TAT + 273.0, 0.2, 0.2);
+ OilPressure_psi = N2 * 0.62;
+ NozzlePosition = Seek(&NozzlePosition, 1.0, 0.8, 0.8);
+ EPR = Seek(&EPR, 1.0, 0.2, 0.2);
+ return 0.0;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
double FGSimTurbine::Run(void)
{
- double idlethrust, milthrust, thrust;
- double N2norm; // 0.0 = idle N2, 1.0 = maximum N2
- idlethrust = MilThrust * ThrustTables[0]->TotalValue();
- milthrust = (MilThrust - idlethrust) * ThrustTables[1]->TotalValue();
+ double idlethrust, milthrust, thrust;
+ double N2norm; // 0.0 = idle N2, 1.0 = maximum N2
+ idlethrust = MilThrust * ThrustTables[0]->TotalValue();
+ milthrust = (MilThrust - idlethrust) * ThrustTables[1]->TotalValue();
+
+ Running = true;
+ Starter = false;
- Running = true;
- Starter = false;
-
- N2 = Seek(&N2, IdleN2 + ThrottleCmd * N2_factor, delay, delay * 3.0);
- N1 = Seek(&N1, IdleN1 + ThrottleCmd * N1_factor, delay, delay * 2.4);
- N2norm = (N2 - IdleN2) / N2_factor;
- thrust = idlethrust + (milthrust * N2norm * N2norm);
- thrust = thrust * (1.0 - BleedDemand);
- FuelFlow_pph = thrust * TSFC;
+ N2 = Seek(&N2, IdleN2 + ThrottleCmd * N2_factor, delay, delay * 3.0);
+ N1 = Seek(&N1, IdleN1 + ThrottleCmd * N1_factor, delay, delay * 2.4);
+ N2norm = (N2 - IdleN2) / N2_factor;
+ thrust = idlethrust + (milthrust * N2norm * N2norm);
+ thrust = thrust * (1.0 - BleedDemand);
+ EGT_degC = TAT + 363.1 + ThrottleCmd * 357.1;
+ OilPressure_psi = N2 * 0.62;
+ OilTemp_degK = Seek(&OilTemp_degK, 366.0, 1.2, 0.1);
+ EPR = 1.0 + thrust/MilThrust;
+
+ if (!Augmentation) {
+ FuelFlow_pph = Seek(&FuelFlow_pph, thrust * TSFC, 1000.0, 100000);
if (FuelFlow_pph < IdleFF) FuelFlow_pph = IdleFF;
- EGT_degC = TAT + 363.1 + ThrottleCmd * 357.1;
- OilPressure_psi = N2 * 0.62;
- OilTemp_degK = Seek(&OilTemp_degK, 366.0, 1.2, 0);
- EPR = 1.0 + thrust/MilThrust;
NozzlePosition = Seek(&NozzlePosition, 1.0 - N2norm, 0.8, 0.8);
- if (Reversed) thrust = thrust * -0.2;
+ }
- if (AugMethod == 1) {
- if ((ThrottleCmd > 0.99) && (N2 > 97.0)) {Augmentation = true;}
- else {Augmentation = false;}
- }
+ if (AugMethod == 1) {
+ if ((ThrottleCmd > 0.99) && (N2 > 97.0)) {Augmentation = true;}
+ else {Augmentation = false;}
+ }
- if ((Augmented == 1) && Augmentation) {
- thrust = MaxThrust * ThrustTables[2]->TotalValue();
- FuelFlow_pph = thrust * ATSFC;
- NozzlePosition = Seek(&NozzlePosition, 1.0, 0.8, 0.8);
- }
+ if ((Augmented == 1) && Augmentation) {
+ thrust = MaxThrust * ThrustTables[2]->TotalValue();
+ FuelFlow_pph = Seek(&FuelFlow_pph, thrust * ATSFC, 5000.0, 10000.0);
+ NozzlePosition = Seek(&NozzlePosition, 1.0, 0.8, 0.8);
+ }
- if ((Injected == 1) && Injection)
- thrust = thrust * ThrustTables[3]->TotalValue();
+ if ((Injected == 1) && Injection)
+ thrust = thrust * ThrustTables[3]->TotalValue();
- ConsumeFuel();
- if (Cutoff) phase = tpOff;
- if (Starved) phase = tpOff;
- return thrust;
+ ConsumeFuel();
+ if (Cutoff) phase = tpOff;
+ if (Starved) phase = tpOff;
+
+ return thrust;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
double FGSimTurbine::SpinUp(void)
{
- Running = false;
- FuelFlow_pph = 0.0;
- N2 = Seek(&N2, 25.18, 3.0, N2/2.0);
- N1 = Seek(&N1, 5.21, 1.0, N1/2.0);
- EGT_degC = TAT;
- OilPressure_psi = N2 * 0.62;
- OilTemp_degK = TAT + 273.0;
- EPR = 1.0;
- NozzlePosition = 1.0;
- return 0.0;
+ Running = false;
+ FuelFlow_pph = 0.0;
+ N2 = Seek(&N2, 25.18, 3.0, N2/2.0);
+ N1 = Seek(&N1, 5.21, 1.0, N1/2.0);
+ EGT_degC = Seek(&EGT_degC, TAT, 11.7, 7.3);
+ OilPressure_psi = N2 * 0.62;
+ OilTemp_degK = Seek(&OilTemp_degK, TAT + 273.0, 0.2, 0.2);
+ EPR = 1.0;
+ NozzlePosition = 1.0;
+
+ return 0.0;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
double FGSimTurbine::Start(void)
{
- if ((N2 > 15.0) && !Starved) { // minimum 15% N2 needed for start
- Cranking = true; // provided for sound effects signal
- if (N2 < IdleN2) {
- N2 = Seek(&N2, IdleN2, 2.0, N2/2.0);
- N1 = Seek(&N1, IdleN1, 1.4, N1/2.0);
- EGT_degC = Seek(&EGT_degC, TAT + 363.1, 21.3, 7.3);
- FuelFlow_pph = Seek(&FuelFlow_pph, IdleFF, 103.7, 103.7);
- OilPressure_psi = N2 * 0.62;
- }
- else {
- phase = tpRun;
- Running = true;
- Starter = false;
- Cranking = false;
- }
+ if ((N2 > 15.0) && !Starved) { // minimum 15% N2 needed for start
+ Cranking = true; // provided for sound effects signal
+ if (N2 < IdleN2) {
+ N2 = Seek(&N2, IdleN2, 2.0, N2/2.0);
+ N1 = Seek(&N1, IdleN1, 1.4, N1/2.0);
+ EGT_degC = Seek(&EGT_degC, TAT + 363.1, 21.3, 7.3);
+ FuelFlow_pph = Seek(&FuelFlow_pph, IdleFF, 103.7, 103.7);
+ OilPressure_psi = N2 * 0.62;
}
- else { // no start if N2 < 15%
- phase = tpOff;
+ else {
+ phase = tpRun;
+ Running = true;
Starter = false;
- }
- return 0.0;
+ Cranking = false;
+ }
+ }
+ else { // no start if N2 < 15%
+ phase = tpOff;
+ Starter = false;
+ }
+
+ return 0.0;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
double FGSimTurbine::Stall(void)
{
- double qbar = Translation->Getqbar();
- EGT_degC = TAT + 903.14;
- FuelFlow_pph = IdleFF;
- N1 = Seek(&N1, qbar/10.0, 0, N1/10.0);
- N2 = Seek(&N2, qbar/15.0, 0, N2/10.0);
- if (ThrottleCmd == 0) phase = tpRun; // clear the stall with throttle
- return 0.0;
+ double qbar = Translation->Getqbar();
+ EGT_degC = TAT + 903.14;
+ FuelFlow_pph = IdleFF;
+ N1 = Seek(&N1, qbar/10.0, 0, N1/10.0);
+ N2 = Seek(&N2, qbar/15.0, 0, N2/10.0);
+ if (ThrottleCmd == 0) phase = tpRun; // clear the stall with throttle
+
+ return 0.0;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGSimTurbine::SetDefaults(void)
{
- Name = "None_Defined";
+ Name = "Not defined";
+ Type = etSimTurbine;
MilThrust = 10000.0;
MaxThrust = 10000.0;
BypassRatio = 0.0;
Augmentation = false;
Injection = false;
Reversed = false;
+ Cutoff = true;
phase = tpOff;
Stalled = false;
Seized = false;
Overtemp = false;
Fire = false;
+ EGT_degC = 0.0;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
bool FGSimTurbine::Load(FGConfigFile *Eng_cfg)
{
- int i;
string token;
+
Name = Eng_cfg->GetValue("NAME");
- cout << Name << endl;
Eng_cfg->GetNextConfigLine();
- *Eng_cfg >> token >> MilThrust;
- *Eng_cfg >> token >> MaxThrust;
- *Eng_cfg >> token >> BypassRatio;
- *Eng_cfg >> token >> TSFC;
- *Eng_cfg >> token >> ATSFC;
- *Eng_cfg >> token >> IdleN1;
- *Eng_cfg >> token >> IdleN2;
- *Eng_cfg >> token >> MaxN1;
- *Eng_cfg >> token >> MaxN2;
- *Eng_cfg >> token >> Augmented;
- *Eng_cfg >> token >> AugMethod;
- *Eng_cfg >> token >> Injected;
- i=0;
- while( Eng_cfg->GetValue() != string("/FG_SIMTURBINE") && i < 10){
- ThrustTables.push_back( new FGCoefficient(FDMExec) );
- ThrustTables.back()->Load(Eng_cfg);
- i++;
+ int counter=0;
+
+ while (Eng_cfg->GetValue() != string("/FG_SIMTURBINE")) {
+ *Eng_cfg >> token;
+
+ if (token[0] == '<') token.erase(0,1); // Tables are read "<TABLE"
+
+ if (token == "MILTHRUST") *Eng_cfg >> MilThrust;
+ else if (token == "MAXTHRUST") *Eng_cfg >> MaxThrust;
+ else if (token == "BYPASSRATIO") *Eng_cfg >> BypassRatio;
+ else if (token == "TSFC") *Eng_cfg >> TSFC;
+ else if (token == "ATSFC") *Eng_cfg >> ATSFC;
+ else if (token == "IDLEN1") *Eng_cfg >> IdleN1;
+ else if (token == "IDLEN2") *Eng_cfg >> IdleN2;
+ else if (token == "MAXN1") *Eng_cfg >> MaxN1;
+ else if (token == "MAXN2") *Eng_cfg >> MaxN2;
+ else if (token == "AUGMENTED") *Eng_cfg >> Augmented;
+ else if (token == "AUGMETHOD") *Eng_cfg >> AugMethod;
+ else if (token == "INJECTED") *Eng_cfg >> Injected;
+ else if (token == "MINTHROTTLE") *Eng_cfg >> MinThrottle;
+ else if (token == "TABLE") {
+ if (counter++ == 0) Debug(2); // print engine specs prior to table read
+ ThrustTables.push_back( new FGCoefficient(FDMExec) );
+ ThrustTables.back()->Load(Eng_cfg);
+ }
+ else cerr << "Unhandled token in Engine config file: " << token << endl;
}
-
- // pre-calculations and initializations
- delay= 60.0 / (BypassRatio + 3.0);
+
+ // Pre-calculations and initializations
+
+ delay = 60.0 / (BypassRatio + 3.0);
N1_factor = MaxN1 - IdleN1;
N2_factor = MaxN2 - IdleN2;
OilTemp_degK = (Auxiliary->GetTotalTemperature() - 491.69) * 0.5555556 + 273.0;
IdleFF = pow(MilThrust, 0.2) * 107.0; // just an estimate
+
return true;
}
if (from == 0) { // Constructor
}
+ if (from == 2) { // called from Load()
+ cout << "\n Engine Name: " << Name << endl;
+ cout << " MilThrust: " << MilThrust << endl;
+ cout << " MaxThrust: " << MaxThrust << endl;
+ cout << " BypassRatio: " << BypassRatio << endl;
+ cout << " TSFC: " << TSFC << endl;
+ cout << " ATSFC: " << ATSFC << endl;
+ cout << " IdleN1: " << IdleN1 << endl;
+ cout << " IdleN2: " << IdleN2 << endl;
+ cout << " MaxN1: " << MaxN1 << endl;
+ cout << " MaxN2: " << MaxN2 << endl;
+ cout << " Augmented: " << Augmented << endl;
+ cout << " AugMethod: " << AugMethod << endl;
+ cout << " Injected: " << Injected << endl;
+ cout << " MinThrottle: " << MinThrottle << endl;
+
+ cout << endl;
+ }
}
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
if (from == 0) cout << "Instantiated: FGSimTurbine" << endl;
projects / flightgear.git / blobdiff