FlightGear next
JSBSim::FGTurbine Class Reference

This class models a turbine engine. More...

#include <FGTurbine.h>

Inherits JSBSim::FGEngine.

Public Types

enum  phaseType {
  tpOff , tpRun , tpSpinUp , tpStart ,
  tpStall , tpSeize , tpTrim
}
 
- Public Types inherited from JSBSim::FGEngine
enum  EngineType {
  etUnknown , etRocket , etPiston , etTurbine ,
  etTurboprop , etElectric
}
 
- Public Types inherited from JSBSim::FGJSBBase
enum  { eL = 1 , eM , eN }
 Moments L, M, N. More...
 
enum  { eP = 1 , eQ , eR }
 Rates P, Q, R. More...
 
enum  { eU = 1 , eV , eW }
 Velocities U, V, W. More...
 
enum  { eX = 1 , eY , eZ }
 Positions X, Y, Z. More...
 
enum  { ePhi = 1 , eTht , ePsi }
 Euler angles Phi, Theta, Psi. More...
 
enum  { eDrag = 1 , eSide , eLift }
 Stability axis forces, Drag, Side force, Lift. More...
 
enum  { eRoll = 1 , ePitch , eYaw }
 Local frame orientation Roll, Pitch, Yaw. More...
 
enum  { eNorth = 1 , eEast , eDown }
 Local frame position North, East, Down. More...
 
enum  { eLat = 1 , eLong , eRad }
 Locations Radius, Latitude, Longitude. More...
 
enum  {
  inNone = 0 , inDegrees , inRadians , inMeters ,
  inFeet
}
 Conversion specifiers. More...
 

Public Member Functions

 FGTurbine (FGFDMExec *Executive, Element *el, int engine_number, struct Inputs &input)
 Constructor.
 
 ~FGTurbine ()
 Destructor.
 
void Calculate (void)
 Calculates the thrust of the engine, and other engine functions.
 
double CalcFuelNeed (void)
 The fuel need is calculated based on power levels and flow rate for that power level.
 
double GetPowerAvailable (void)
 
double Seek (double *var, double target, double accel, double decel)
 A lag filter.
 
phaseType GetPhase (void)
 
bool GetOvertemp (void) const
 
bool GetInjection (void) const
 
bool GetFire (void) const
 
bool GetAugmentation (void) const
 
bool GetReversed (void) const
 
bool GetCutoff (void) const
 
int GetIgnition (void) const
 
double GetInlet (void) const
 
double GetNozzle (void) const
 
double GetBleedDemand (void) const
 
double GetN1 (void) const
 
double GetN2 (void) const
 
double GetEPR (void) const
 
double GetEGT (void) const
 
double GetMaxN1 (void) const
 
double GetMaxN2 (void) const
 
double getOilPressure_psi () const
 
double getOilTemp_degF (void)
 
double GetInjectionTimer (void) const
 
double GetInjWaterNorm (void) const
 
double GetInjN1increment (void) const
 
double GetInjN2increment (void) const
 
void SetInjection (bool injection)
 
void SetIgnition (int ignition)
 
void SetAugmentation (bool augmentation)
 
void SetPhase (phaseType p)
 
void SetEPR (double epr)
 
void SetBleedDemand (double bleedDemand)
 
void SetReverse (bool reversed)
 
void SetCutoff (bool cutoff)
 
void SetMaxN1 (double maxn1)
 
void SetMaxN2 (double maxn2)
 
void SetInjectionTimer (double injtimer)
 
void SetInjWaterNorm (double injwater)
 
void SetInjN1increment (double injN1inc)
 
void SetInjN2increment (double injN2inc)
 
int InitRunning (void)
 
void ResetToIC (void)
 Resets the Engine parameters to the initial conditions.
 
std::string GetEngineLabels (const std::string &delimiter)
 
std::string GetEngineValues (const std::string &delimiter)
 
- Public Member Functions inherited from JSBSim::FGEngine
 FGEngine (int engine_number, struct Inputs &input)
 
 ~FGEngine () override
 
EngineType GetType (void) const
 
virtual const std::string & GetName (void) const
 
virtual double GetThrottleMin (void) const
 
virtual double GetThrottleMax (void) const
 
virtual bool GetStarter (void) const
 
virtual double getFuelFlow_gph () const
 
virtual double getFuelFlow_pph () const
 
virtual double GetFuelFlowRate (void) const
 
virtual double GetFuelFlowRateGPH (void) const
 
virtual double GetFuelUsedLbs (void) const
 
virtual bool GetStarved (void) const
 
virtual bool GetRunning (void) const
 
virtual bool GetCranking (void) const
 
virtual void SetStarved (bool tt)
 
virtual void SetStarved (void)
 
virtual void SetRunning (bool bb)
 
virtual void SetName (const std::string &name)
 
virtual void SetFuelFreeze (bool f)
 
virtual void SetFuelDensity (double d)
 
virtual void SetStarter (bool s)
 
virtual double GetThrust (void) const
 
virtual double CalcOxidizerNeed (void)
 
virtual const FGColumnVector3GetBodyForces (void)
 
virtual const FGColumnVector3GetMoments (void)
 
void LoadThruster (FGFDMExec *exec, Element *el)
 
FGThrusterGetThruster (void) const
 
unsigned int GetSourceTank (unsigned int i) const
 
size_t GetNumSourceTanks () const
 
void LoadThrusterInputs ()
 
- Public Member Functions inherited from JSBSim::FGModelFunctions
virtual ~FGModelFunctions ()
 
void RunPreFunctions (void)
 
void RunPostFunctions (void)
 
bool Load (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
void PreLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
void PostLoad (Element *el, FGFDMExec *fdmex, std::string prefix="")
 
std::string GetFunctionStrings (const std::string &delimeter) const
 Gets the strings for the current set of functions.
 
std::string GetFunctionValues (const std::string &delimeter) const
 Gets the function values.
 
FGFunctionGetPreFunction (const std::string &name)
 Get one of the "pre" function.
 
- Public Member Functions inherited from JSBSim::FGJSBBase
 FGJSBBase ()
 Constructor for FGJSBBase.
 
virtual ~FGJSBBase ()
 Destructor for FGJSBBase.
 
void PutMessage (const Message &msg)
 Places a Message structure on the Message queue.
 
void PutMessage (const std::string &text)
 Creates a message with the given text and places it on the queue.
 
void PutMessage (const std::string &text, bool bVal)
 Creates a message with the given text and boolean value and places it on the queue.
 
void PutMessage (const std::string &text, int iVal)
 Creates a message with the given text and integer value and places it on the queue.
 
void PutMessage (const std::string &text, double dVal)
 Creates a message with the given text and double value and places it on the queue.
 
int SomeMessages (void) const
 Reads the message on the queue (but does not delete it).
 
void ProcessMessage (void)
 Reads the message on the queue and removes it from the queue.
 
MessageProcessNextMessage (void)
 Reads the next message on the queue and removes it from the queue.
 
void disableHighLighting (void)
 Disables highlighting in the console output.
 

Friends

class FGSpoolUp
 

Additional Inherited Members

static const std::string & GetVersion (void)
 Returns the version number of JSBSim.
 
static constexpr double KelvinToFahrenheit (double kelvin)
 Converts from degrees Kelvin to degrees Fahrenheit.
 
static constexpr double CelsiusToRankine (double celsius)
 Converts from degrees Celsius to degrees Rankine.
 
static constexpr double RankineToCelsius (double rankine)
 Converts from degrees Rankine to degrees Celsius.
 
static constexpr double KelvinToRankine (double kelvin)
 Converts from degrees Kelvin to degrees Rankine.
 
static constexpr double RankineToKelvin (double rankine)
 Converts from degrees Rankine to degrees Kelvin.
 
static constexpr double FahrenheitToCelsius (double fahrenheit)
 Converts from degrees Fahrenheit to degrees Celsius.
 
static constexpr double CelsiusToFahrenheit (double celsius)
 Converts from degrees Celsius to degrees Fahrenheit.
 
static constexpr double CelsiusToKelvin (double celsius)
 Converts from degrees Celsius to degrees Kelvin.
 
static constexpr double KelvinToCelsius (double kelvin)
 Converts from degrees Kelvin to degrees Celsius.
 
static constexpr double FeetToMeters (double measure)
 Converts from feet to meters.
 
static double PitotTotalPressure (double mach, double p)
 Compute the total pressure in front of the Pitot tube.
 
static double MachFromImpactPressure (double qc, double p)
 Compute the Mach number from the differential pressure (qc) and the static pressure.
 
static double VcalibratedFromMach (double mach, double p)
 Calculate the calibrated airspeed from the Mach number.
 
static double MachFromVcalibrated (double vcas, double p)
 Calculate the Mach number from the calibrated airspeed.Based on the formulas in the US Air Force Aircraft Performance Flight Testing Manual (AFFTC-TIH-99-01).
 
static bool EqualToRoundoff (double a, double b)
 Finite precision comparison.
 
static bool EqualToRoundoff (float a, float b)
 Finite precision comparison.
 
static bool EqualToRoundoff (float a, double b)
 Finite precision comparison.
 
static bool EqualToRoundoff (double a, float b)
 Finite precision comparison.
 
static constexpr double Constrain (double min, double value, double max)
 Constrain a value between a minimum and a maximum value.
 
static constexpr double sign (double num)
 
static double GaussianRandomNumber (void)
 
- Public Attributes inherited from JSBSim::FGEngine
struct Inputsin
 
- Static Public Attributes inherited from JSBSim::FGJSBBase
static char highint [5] = {27, '[', '1', 'm', '\0' }
 highlights text
 
static char halfint [5] = {27, '[', '2', 'm', '\0' }
 low intensity text
 
static char normint [6] = {27, '[', '2', '2', 'm', '\0' }
 normal intensity text
 
static char reset [5] = {27, '[', '0', 'm', '\0' }
 resets text properties
 
static char underon [5] = {27, '[', '4', 'm', '\0' }
 underlines text
 
static char underoff [6] = {27, '[', '2', '4', 'm', '\0' }
 underline off
 
static char fgblue [6] = {27, '[', '3', '4', 'm', '\0' }
 blue text
 
static char fgcyan [6] = {27, '[', '3', '6', 'm', '\0' }
 cyan text
 
static char fgred [6] = {27, '[', '3', '1', 'm', '\0' }
 red text
 
static char fggreen [6] = {27, '[', '3', '2', 'm', '\0' }
 green text
 
static char fgdef [6] = {27, '[', '3', '9', 'm', '\0' }
 default text
 
static short debug_lvl = 1
 
- Protected Member Functions inherited from JSBSim::FGEngine
bool Load (FGFDMExec *exec, Element *el)
 
void Debug (int from)
 
- Protected Member Functions inherited from JSBSim::FGModelFunctions
virtual bool InitModel (void)
 
static std::string CreateIndexedPropertyName (const std::string &Property, int index)
 
- Protected Attributes inherited from JSBSim::FGEngine
std::string Name
 
const int EngineNumber
 
EngineType Type
 
double SLFuelFlowMax
 
double MaxThrottle
 
double MinThrottle
 
double FuelExpended
 
double FuelFlowRate
 
double PctPower
 
bool Starter
 
bool Starved
 
bool Running
 
bool Cranking
 
bool FuelFreeze
 
double FuelFlow_gph
 
double FuelFlow_pph
 
double FuelUsedLbs
 
double FuelDensity
 
FGThrusterThruster
 
std::vector< int > SourceTanks
 
- Protected Attributes inherited from JSBSim::FGModelFunctions
std::vector< FGFunction * > PreFunctions
 
std::vector< FGFunction * > PostFunctions
 
FGPropertyReader LocalProperties
 
static Message localMsg
 
static std::queue< MessageMessages
 
static unsigned int messageId = 0
 
static constexpr double radtodeg = 180. / 3.14159265358979323846
 
static constexpr double degtorad = 3.14159265358979323846 / 180.
 
static constexpr double hptoftlbssec = 550.0
 
static constexpr double psftoinhg = 0.014138
 
static constexpr double psftopa = 47.88
 
static constexpr double ktstofps = 1.68781
 
static constexpr double fpstokts = 1.0 / ktstofps
 
static constexpr double inchtoft = 1.0/12.0
 
static constexpr double fttom = 0.3048
 
static constexpr double m3toft3 = 1.0/(fttom*fttom*fttom)
 
static constexpr double in3tom3 = inchtoft*inchtoft*inchtoft/m3toft3
 
static constexpr double inhgtopa = 3386.38
 
static constexpr double slugtolb = 32.174049
 Note that definition of lbtoslug by the inverse of slugtolb and not to a different constant you can also get from some tables will make lbtoslug*slugtolb == 1 up to the magnitude of roundoff.
 
static constexpr double lbtoslug = 1.0/slugtolb
 
static constexpr double kgtolb = 2.20462
 
static constexpr double kgtoslug = 0.06852168
 
static const std::string needed_cfg_version = "2.0"
 
static const std::string JSBSim_version = JSBSIM_VERSION " " __DATE__ " " __TIME__
 
static int gaussian_random_number_phase = 0
 

Detailed Description

This class models a turbine engine.

Based on Jon Berndt's FGTurbine module. Here the term "phase" signifies the engine's mode of operation. At any given time the engine is in only one phase. At simulator startup the engine will be placed in the Trim phase in order to provide a simplified thrust value without throttle lag. When trimming is complete the engine will go to the Off phase, unless the value FGEngine::Running has been previously set to true, in which case the engine will go to the Run phase. Once an engine is in the Off phase the full starting procedure (or airstart) must be used to get it running.

  • STARTING (on ground):
    1. Set the control FGEngine::Starter to true. The engine will spin up to a maximum of about %25 N2 (%5.2 N1). This value may be changed using the <startnX> parameter. This simulates the action of a pneumatic starter.
    2. After reaching %15 N2 set the control FGEngine::Cutoff to false. If fuel is available the engine will now accelerate to idle. The starter will automatically be set to false after the start cycle.
  • STARTING (in air):

    1. Increase speed to obtain a minimum of %15 N2. If this is not possible, the starter may be used to assist.
    2. Place the control FGEngine::Cutoff to false.

    Ignition is assumed to be on anytime the Cutoff control is set to false, therefore a separate ignition system is not modeled.

Configuration File Format:

<turbine_engine name="{string}">
<milthrust unit="{LBS | N}"> {number} </milthrust>
<maxthrust unit="{LBS | N}"> {number} </maxthrust>
<bypassratio> {number} </bypassratio>
<bleed> {number} </bleed>
<tsfc> {number} </tsfc>
<atsfc> {number} </atsfc>
<ignitionn1> {number} </ignitionn1>
<ignitionn2> {number} </ignitionn2>
<idlen1> {number} </idlen1>
<idlen2> {number} </idlen2>
<n1spinup> {number} </n1spinup>
<n2spinup> {number} </n2spinup>
<n1startrate> {number} </n1startrate>
<n2startrate> {number} </n2startrate>
<n1spindown> {number} </n1spindown>
<n2spindown> {number} </n2spindown>
<maxn1> {number} </maxn1>
<maxn2> {number} </maxn2>
<augmented> {0 | 1} </augmented>
<augmethod> {0 | 1 | 2} </augmethod>
<injected> {0 | 1} </injected>
<injection-time> {number} </injection-time>
<disable-windmill> {0 | 1}</disable-windmill>
</turbine_engine>
const char * name

Definition of the turbine engine configuration file parameters:

  milthrust   - Maximum thrust, static, at sea level.
  maxthrust   - Afterburning thrust, static, at sea level.
  bypassratio - Ratio of bypass air flow to core air flow.
  bleed       - Thrust reduction factor due to losses (0.0 to 1.0).
  tsfc        - Thrust-specific fuel consumption at cruise, lbm/hr/lbf
  atsfc       - Afterburning TSFC, lbm/hr/lbf
  ignitionn1  - Fan rotor rpm (% of max) while starting
  ignitionn2  - Core rotor rpm (% of max) while starting
  idlen1      - Fan rotor rpm (% of max) at idle
  idlen2      - Core rotor rpm (% of max) at idle
  n1spinup    - Fan rotor rpm starter acceleration to ignitionn1 value (default 1.0)
  n2spinup    - Core rotor rpm starter acceleration to ignitionn2 value (default 3.0)
  n1startrate - Fan rotor rpm time taken to accelerate from ignitionn1 to idlen1 value (default 1.4)
  n2startrate - Core rotor rpm time taken to accelerate to ignitionn2 idlen2 value (default 2.0)
  n1spindown  - Factor used in calculation for fan rotor time to spool down to zero (default 2.0)
  n2spindown  - Factor used in calculation for core rotor time to spool down to zero (default 2.0)
  maxn1       - Fan rotor rpm (% of max) at full throttle 
  maxn2       - Core rotor rpm (% of max) at full throttle
  augmented
              0 = afterburner not installed
              1 = afterburner installed
  augmethod
              0 = afterburner activated by property /engines/engine[n]/augmentation
              1 = afterburner activated by pushing throttle above 99% position
              2 = throttle range is expanded in the FCS, and values above 1.0 are afterburner range
  injected
              0 = Water injection not installed
              1 = Water injection installed
  injection-time - Time, in seconds, of water injection duration 
  InjN1increment - % increase in N1 when injection is taking place
  InjN2increment - % increase in N2 when injection is taking place
  disable-windmill - flag that disables engine windmilling when off if true

NOTES:


    Bypass ratio is used only to estimate engine acceleration time.  The
    effect of bypass ratio on engine efficiency is already included in
    the TSFC value.  Feel free to set this parameter (even for turbojets) to
    whatever value gives a desired spool-up rate. Default value is 0.

    The bleed factor is multiplied by thrust to give a resulting thrust
    after losses.  This can represent losses due to bleed, or any other cause.
    Default value is 0.  A common value would be 0.04.

    Nozzle position, for variable area exhaust nozzles, is provided for users
    needing to drive a nozzle gauge or animate a virtual nozzle.

    This model can only be used with the "direct" thruster.  See the file:
    /engine/direct.xml
Author
David P. Culp

Definition at line 154 of file FGTurbine.h.

Member Enumeration Documentation

◆ phaseType

Enumerator
tpOff 
tpRun 
tpSpinUp 
tpStart 
tpStall 
tpSeize 
tpTrim 

Definition at line 165 of file FGTurbine.h.

Constructor & Destructor Documentation

◆ FGTurbine()

JSBSim::FGTurbine::FGTurbine ( FGFDMExec * Executive,
Element * el,
int engine_number,
struct Inputs & input )

Constructor.

Parameters
Executivepointer to executive structure
elpointer to the XML element representing the turbine engine
engine_numberengine number

Definition at line 59 of file FGTurbine.cpp.

◆ ~FGTurbine()

JSBSim::FGTurbine::~FGTurbine ( )

Destructor.

Definition at line 86 of file FGTurbine.cpp.

Member Function Documentation

◆ CalcFuelNeed()

double JSBSim::FGTurbine::CalcFuelNeed ( void )
virtual

The fuel need is calculated based on power levels and flow rate for that power level.

It is also turned from a rate into an actual amount (pounds) by multiplying it by the delta T and the rate.

Returns
Total fuel requirement for this engine in pounds.

Reimplemented from JSBSim::FGEngine.

Definition at line 397 of file FGTurbine.cpp.

◆ Calculate()

void JSBSim::FGTurbine::Calculate ( void )
virtual

Calculates the thrust of the engine, and other engine functions.

Implements JSBSim::FGEngine.

Definition at line 122 of file FGTurbine.cpp.

◆ GetAugmentation()

bool JSBSim::FGTurbine::GetAugmentation ( void ) const
inline

Definition at line 189 of file FGTurbine.h.

◆ GetBleedDemand()

double JSBSim::FGTurbine::GetBleedDemand ( void ) const
inline

Definition at line 196 of file FGTurbine.h.

◆ GetCutoff()

bool JSBSim::FGTurbine::GetCutoff ( void ) const
inline

Definition at line 191 of file FGTurbine.h.

◆ GetEGT()

double JSBSim::FGTurbine::GetEGT ( void ) const
inline

Definition at line 200 of file FGTurbine.h.

◆ GetEngineLabels()

string JSBSim::FGTurbine::GetEngineLabels ( const std::string & delimiter)
virtual

Implements JSBSim::FGEngine.

Definition at line 535 of file FGTurbine.cpp.

◆ GetEngineValues()

string JSBSim::FGTurbine::GetEngineValues ( const std::string & delimiter)
virtual

Implements JSBSim::FGEngine.

Definition at line 548 of file FGTurbine.cpp.

◆ GetEPR()

double JSBSim::FGTurbine::GetEPR ( void ) const
inline

Definition at line 199 of file FGTurbine.h.

◆ GetFire()

bool JSBSim::FGTurbine::GetFire ( void ) const
inline

Definition at line 188 of file FGTurbine.h.

◆ GetIgnition()

int JSBSim::FGTurbine::GetIgnition ( void ) const
inline

Definition at line 192 of file FGTurbine.h.

◆ GetInjection()

bool JSBSim::FGTurbine::GetInjection ( void ) const
inline

Definition at line 187 of file FGTurbine.h.

◆ GetInjectionTimer()

double JSBSim::FGTurbine::GetInjectionTimer ( void ) const
inline

Definition at line 206 of file FGTurbine.h.

◆ GetInjN1increment()

double JSBSim::FGTurbine::GetInjN1increment ( void ) const
inline

Definition at line 208 of file FGTurbine.h.

◆ GetInjN2increment()

double JSBSim::FGTurbine::GetInjN2increment ( void ) const
inline

Definition at line 209 of file FGTurbine.h.

◆ GetInjWaterNorm()

double JSBSim::FGTurbine::GetInjWaterNorm ( void ) const
inline

Definition at line 207 of file FGTurbine.h.

◆ GetInlet()

double JSBSim::FGTurbine::GetInlet ( void ) const
inline

Definition at line 194 of file FGTurbine.h.

◆ GetMaxN1()

double JSBSim::FGTurbine::GetMaxN1 ( void ) const
inline

Definition at line 202 of file FGTurbine.h.

◆ GetMaxN2()

double JSBSim::FGTurbine::GetMaxN2 ( void ) const
inline

Definition at line 203 of file FGTurbine.h.

◆ GetN1()

double JSBSim::FGTurbine::GetN1 ( void ) const
inline

Definition at line 197 of file FGTurbine.h.

◆ GetN2()

double JSBSim::FGTurbine::GetN2 ( void ) const
inline

Definition at line 198 of file FGTurbine.h.

◆ GetNozzle()

double JSBSim::FGTurbine::GetNozzle ( void ) const
inline

Definition at line 195 of file FGTurbine.h.

◆ getOilPressure_psi()

double JSBSim::FGTurbine::getOilPressure_psi ( ) const
inline

Definition at line 204 of file FGTurbine.h.

◆ getOilTemp_degF()

double JSBSim::FGTurbine::getOilTemp_degF ( void )
inline

Definition at line 205 of file FGTurbine.h.

◆ GetOvertemp()

bool JSBSim::FGTurbine::GetOvertemp ( void ) const
inline

Definition at line 186 of file FGTurbine.h.

◆ GetPhase()

phaseType JSBSim::FGTurbine::GetPhase ( void )
inline

Definition at line 184 of file FGTurbine.h.

◆ GetPowerAvailable()

double JSBSim::FGTurbine::GetPowerAvailable ( void )
virtual

Reimplemented from JSBSim::FGEngine.

Definition at line 407 of file FGTurbine.cpp.

◆ GetReversed()

bool JSBSim::FGTurbine::GetReversed ( void ) const
inline

Definition at line 190 of file FGTurbine.h.

◆ InitRunning()

int JSBSim::FGTurbine::InitRunning ( void )
virtual

Reimplemented from JSBSim::FGEngine.

Definition at line 600 of file FGTurbine.cpp.

◆ ResetToIC()

void JSBSim::FGTurbine::ResetToIC ( void )
virtual

Resets the Engine parameters to the initial conditions.

Reimplemented from JSBSim::FGEngine.

Definition at line 101 of file FGTurbine.cpp.

◆ Seek()

double JSBSim::FGTurbine::Seek ( double * var,
double target,
double accel,
double decel )

A lag filter.

Used to control the rate at which values are allowed to change.

Parameters
vara pointer to a variable of type double
targetthe desired (target) value
accelthe rate, per second, the value may increase
decelthe rate, per second, the value may decrease

Definition at line 416 of file FGTurbine.cpp.

◆ SetAugmentation()

void JSBSim::FGTurbine::SetAugmentation ( bool augmentation)
inline

Definition at line 213 of file FGTurbine.h.

◆ SetBleedDemand()

void JSBSim::FGTurbine::SetBleedDemand ( double bleedDemand)
inline

Definition at line 216 of file FGTurbine.h.

◆ SetCutoff()

void JSBSim::FGTurbine::SetCutoff ( bool cutoff)
inline

Definition at line 218 of file FGTurbine.h.

◆ SetEPR()

void JSBSim::FGTurbine::SetEPR ( double epr)
inline

Definition at line 215 of file FGTurbine.h.

◆ SetIgnition()

void JSBSim::FGTurbine::SetIgnition ( int ignition)
inline

Definition at line 212 of file FGTurbine.h.

◆ SetInjection()

void JSBSim::FGTurbine::SetInjection ( bool injection)
inline

Definition at line 211 of file FGTurbine.h.

◆ SetInjectionTimer()

void JSBSim::FGTurbine::SetInjectionTimer ( double injtimer)
inline

Definition at line 221 of file FGTurbine.h.

◆ SetInjN1increment()

void JSBSim::FGTurbine::SetInjN1increment ( double injN1inc)
inline

Definition at line 223 of file FGTurbine.h.

◆ SetInjN2increment()

void JSBSim::FGTurbine::SetInjN2increment ( double injN2inc)
inline

Definition at line 224 of file FGTurbine.h.

◆ SetInjWaterNorm()

void JSBSim::FGTurbine::SetInjWaterNorm ( double injwater)
inline

Definition at line 222 of file FGTurbine.h.

◆ SetMaxN1()

void JSBSim::FGTurbine::SetMaxN1 ( double maxn1)
inline

Definition at line 219 of file FGTurbine.h.

◆ SetMaxN2()

void JSBSim::FGTurbine::SetMaxN2 ( double maxn2)
inline

Definition at line 220 of file FGTurbine.h.

◆ SetPhase()

void JSBSim::FGTurbine::SetPhase ( phaseType p)
inline

Definition at line 214 of file FGTurbine.h.

◆ SetReverse()

void JSBSim::FGTurbine::SetReverse ( bool reversed)
inline

Definition at line 217 of file FGTurbine.h.

Friends And Related Symbol Documentation

◆ FGSpoolUp

friend class FGSpoolUp
friend

Definition at line 310 of file FGTurbine.h.


The documentation for this class was generated from the following files: