Author: Jon S. Berndt
Date started: 09/12/2000
- ------------- Copyright (C) 2000 Jon S. Berndt (jsb@hal-pc.org) --------------
+ ------------- Copyright (C) 2000 Jon S. Berndt (jon@jsbsim.org) --------------
This program is free software; you can redistribute it and/or modify it under
the terms of the GNU Lesser General Public License as published by the Free Software
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGEngine.h"
-#include <math/FGTable.h>
-#include <input_output/FGXMLElement.h>
+#include "math/FGTable.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-#define ID_PISTON "$Id$";
+#define ID_PISTON "$Id: FGPiston.h,v 1.26 2011/03/10 01:35:25 dpculp Exp $";
#define FG_MAX_BOOST_SPEEDS 3
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@code
<piston_engine name="{string}">
- <minmp unit="{INHG | PA | ATM}"> {number} </minmp> <!-- Depricated -->
+ <minmp unit="{INHG | PA | ATM}"> {number} </minmp>
<maxmp unit="{INHG | PA | ATM}"> {number} </maxmp>
<displacement unit="{IN3 | LTR | CC}"> {number} </displacement>
<bore unit="{IN | M}"> {number} </bore>
<stroke unit="{IN | M}"> {number} </stroke>
<cylinders> {number} </cylinders>
+ <cylinder-head-mass unit="{KG | LBS}"> {number} </cylinder-head-mass>
<compression-ratio> {number} </compression-ratio>
<sparkfaildrop> {number} </sparkfaildrop>
<maxhp unit="{HP | WATTS}"> {number} </maxhp>
<maxrpm> {number} </maxrpm>
<maxthrottle> {number} </maxthrottle>
<minthrottle> {number} </minthrottle>
- <bsfc unit="{LBS/HP*HR | "KG/KW*HR"}"> {number} </bsft>
- <volumetric_efficiency> {number} </volumetric_efficiency>
+ <bsfc unit="{LBS/HP*HR | "KG/KW*HR"}"> {number} </bsfc>
+ <volumetric-efficiency> {number} </volumetric-efficiency>
+ <dynamic-fmep unit="{INHG | PA | ATM}"> {number} </dynamic-fmep>
+ <static-fmep unit="{INHG | PA | ATM}"> {number} </static-fmep>
<numboostspeeds> {number} </numboostspeeds>
<boostoverride> {0 | 1} </boostoverride>
+ <boostmanual> {0 | 1} </boostmanual>
<ratedboost1 unit="{INHG | PA | ATM}"> {number} </ratedboost1>
<ratedpower1 unit="{HP | WATTS}"> {number} </ratedpower1>
<ratedrpm1> {number} </ratedrpm1>
<ratedrpm3> {number} </ratedrpm3>
<ratedaltitude3 unit="{FT | M}"> {number} </ratedaltitude3>
<takeoffboost unit="{INHG | PA | ATM}"> {number} </takeoffboost>
+ <air-intake-impedance-factor> {number} </air-intake-impedance-factor>
+ <ram-air-factor> {number} </ram-air-factor>
+ <cooling-factor> {number} </cooling-factor>
</piston_engine>
@endcode
some way of getting the boost control cutout lever position (on or off)
from FlightGear first.
+ - BOOSTMANUAL - whether a multispeed supercharger will manually or
+ automatically shift boost speeds. On manual shifting the boost speeds
+ is accomplished by controling propulsion/engine/boostspeed
+
- The next items are all appended with either 1, 2 or 3 depending on which
boost speed they refer to, eg RATEDBOOST1. The rated values seems to have
been a common convention at the time to express the maximum continuously
config file (and is above RATEDBOOST1), then the throttle position is
interpreted as:
- - 0 to 0.95 : idle manifold pressure to rated boost (where attainable)
- - 0.96, 0.97, 0.98 : rated boost (where attainable).
+ - 0 to 0.98 : idle manifold pressure to rated boost (where attainable)
- 0.99, 1.0 : takeoff boost (where attainable).
A typical takeoff boost for an earlyish Merlin was about 12psi, compared
@author Dave Luff (engine operational code)
@author David Megginson (initial porting and additional code)
@author Ron Jensen (additional engine code)
- @version $Id$
+ @version $Id: FGPiston.h,v 1.26 2011/03/10 01:35:25 dpculp Exp $
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
/// Destructor
~FGPiston();
- string GetEngineLabels(string delimeter);
- string GetEngineValues(string delimeter);
+ std::string GetEngineLabels(const std::string& delimiter);
+ std::string GetEngineValues(const std::string& delimiter);
- double Calculate(void);
- double GetPowerAvailable(void) {return PowerAvailable;}
+ void Calculate(void);
+ double GetPowerAvailable(void) const {return (HP * hptoftlbssec);}
double CalcFuelNeed(void);
void ResetToIC(void);
void SetMagnetos(int magnetos) {Magnetos = magnetos;}
- double GetEGT(void) { return EGT_degC; }
- int GetMagnetos(void) {return Magnetos;}
+ double GetEGT(void) const { return EGT_degC; }
+ int GetMagnetos(void) const {return Magnetos;}
- double getExhaustGasTemp_degF(void) {return KelvinToFahrenheit(ExhaustGasTemp_degK);}
+ double getExhaustGasTemp_degF(void) const {return KelvinToFahrenheit(ExhaustGasTemp_degK);}
double getManifoldPressure_inHg(void) const {return ManifoldPressure_inHg;}
- double getCylinderHeadTemp_degF(void) {return KelvinToFahrenheit(CylinderHeadTemp_degK);}
+ double getCylinderHeadTemp_degF(void) const {return KelvinToFahrenheit(CylinderHeadTemp_degK);}
double getOilPressure_psi(void) const {return OilPressure_psi;}
- double getOilTemp_degF (void) {return KelvinToFahrenheit(OilTemp_degK);}
- double getRPM(void) {return RPM;}
+ double getOilTemp_degF (void) const {return KelvinToFahrenheit(OilTemp_degK);}
+ double getRPM(void) const {return RPM;}
protected:
- double ThrottleAngle;
private:
int crank_counter;
double IndicatedHorsePower;
double PMEP;
double FMEP;
- double SpeedSlope;
- double SpeedIntercept;
- double AltitudeSlope;
- double PowerAvailable;
+ double FMEPDynamic;
+ double FMEPStatic;
// timestep
double dt;
const double calorific_value_fuel; // W/Kg (approximate)
const double Cp_air; // J/KgK
const double Cp_fuel; // J/KgK
+ const double standard_pressure; //Pa
+
FGTable *Lookup_Combustion_Efficiency;
FGTable *Mixture_Efficiency_Correlation;
double Bore; // inches
double Stroke; // inches
double Cylinders; // number
- double CompressionRatio; // number
+ double CylinderHeadMass; // kilograms
+ double CompressionRatio; // number
+ double Z_airbox; // number representing intake impediance before the throttle
+ double Z_throttle; // number representing slope of throttle impediance
+ double PeakMeanPistonSpeed_fps; // ft/sec speed where intake valves begin to choke. Typically 33-50 fps
+ double RatedMeanPistonSpeed_fps; // ft/sec derived from MaxRPM and stroke.
+ double Ram_Air_Factor; // number
double StarterHP; // initial horsepower of starter motor
int BoostSpeeds; // Number of super/turbocharger boost speeds - zero implies no turbo/supercharging.
int BoostSpeed; // The current boost-speed (zero-based).
bool Boosted; // Set true for boosted engine.
+ int BoostManual; // The raw value read in from the config file - should be 1 or 0 - see description below.
+ bool bBoostManual; // Set true if pilot must manually control the boost speed.
int BoostOverride; // The raw value read in from the config file - should be 1 or 0 - see description below.
bool bBoostOverride; // Set true if pilot override of the boost regulator was fitted.
// (Typically called 'war emergency power').
double minMAP; // Pa
double maxMAP; // Pa
double MAP; // Pa
+ double TMAP; // Pa - throttle manifold pressure e.g. before the supercharger boost
double ISFC; // Indicated specific fuel consumption [lbs/horsepower*hour
//
// Inputs (in addition to those in FGEngine).
//
double p_amb; // Pascals
+ double p_ram; // Pascals
double T_amb; // degrees Kelvin
double RPM; // revolutions per minute
double IAS; // knots
+ double Cooling_Factor; // normal
bool Magneto_Left;
bool Magneto_Right;
int Magnetos;
projects / flightgear.git / blobdiff