Fix stall widths for the "auxilliary" (reverse flow) stalls so they

[flightgear.git] / src / FDM / JSBSim / FGAtmosphere.h

diff --git a/src/FDM/JSBSim/FGAtmosphere.h b/src/FDM/JSBSim/FGAtmosphere.h
index 7c8aec696688f7ba4fd7e1d3a01610908a24e5e7..711057f75742a846829eb3ca3df1c8f30f99a571 100644 (file)
--- a/src/FDM/JSBSim/FGAtmosphere.h
+++ b/src/FDM/JSBSim/FGAtmosphere.h
@@ -28,7 +28,7 @@ HISTORY
 --------------------------------------------------------------------------------
 11/24/98   JSB   Created
 07/23/99   TP    Added implementation of 1959 Standard Atmosphere
-                 Moved calculation of Mach number to FGTranslation
+                 Moved calculation of Mach number to FGPropagate
                  Updated to '76 model
  
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@@ -92,6 +92,8 @@ public:
   inline double GetDensity(void)  const {return *density;}
   /// Returns the pressure in psf.
   inline double GetPressure(void)  const {return *pressure;}
+  /// Returns the pressure at an arbitrary altitude in psf
+  double GetPressure(double alt);
   /// Returns the speed of sound in ft/sec.
   inline double GetSoundSpeed(void) const {return soundspeed;}
 
@@ -127,6 +129,19 @@ public:
   /// Provides the external atmosphere model with an interface to set the pressure.
   inline void SetExPressure(double p)     { exPressure=p; }
 
+  /// Sets the temperature deviation at sea-level in degrees Fahrenheit
+  inline void SetSLTempDev(double d)  { T_dev_sl = d; }
+  /// Gets the temperature deviation at sea-level in degrees Fahrenheit
+  inline double GetSLTempDev(void) const { return T_dev_sl; }
+  /// Sets the current delta-T in degrees Fahrenheit
+  inline void SetDeltaT(double d)  { delta_T = d; } 
+  /// Gets the current delta-T in degrees Fahrenheit
+  inline double GetDeltaT(void) const  { return delta_T; } 
+  /// Gets the at-altitude temperature deviation in degrees Fahrenheit
+  inline double GetTempDev(void) const { return T_dev; }
+  /// Gets the density altitude in feet
+  inline double GetDensityAltitude(void) const { return density_altitude; }
+
   /// Sets the wind components in NED frame.
   inline void SetWindNED(double wN, double wE, double wD) { vWindNED(1)=wN; vWindNED(2)=wE; vWindNED(3)=wD;}
 
@@ -162,6 +177,7 @@ protected:
   bool useExternal;
   double exTemperature,exDensity,exPressure;
   double intTemperature, intDensity, intPressure;
+  double T_dev_sl, T_dev, delta_T, density_altitude;
   
   double MagnitudedAccelDt, MagnitudeAccel, Magnitude;
   double TurbGain;