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

[flightgear.git] / src / FDM / YASim / Propeller.hpp

diff --git a/src/FDM/YASim/Propeller.hpp b/src/FDM/YASim/Propeller.hpp
index 2e4d3f565add50ee638f778cf5ba7029554abbe0..5a5905e2fc26382b7e77198a0b7f5afc75486b9e 100644 (file)
--- a/src/FDM/YASim/Propeller.hpp
+++ b/src/FDM/YASim/Propeller.hpp
@@ -20,19 +20,28 @@ public:
 
     void modPitch(float mod);
 
+    void setPropPitch(float proppitch);
+
+    void setPropFeather(int state);
+
+    void setManualPitch();
+
     void calc(float density, float v, float omega,
              float* thrustOut, float* torqueOut);
 
 private:
     float _r;           // characteristic radius
-    float _J0;          // zero-thrust advance ratio
+    float _j0;          // zero-thrust advance ratio
     float _baseJ0;      //  ... uncorrected for prop advance
-    float _F0;          // thrust coefficient
+    float _f0;          // thrust coefficient
     float _etaC;        // Peak efficiency
     float _lambdaPeak;  // constant, ~0.759835;
     float _beta;        // constant, ~1.48058;
     float _tc0;         // thrust "coefficient" at takeoff
     bool  _matchTakeoff; // Does _tc0 mean anything?
+    bool  _manual;      // manual pitch mode
+    float _proppitch;   // prop pitch control setting (0 ~ 1.0)
+    float _propfeather; // prop feather control setting (0 = norm, 1 = feather)
 };
 
 }; // namespace yasim