Frederic Bouvier:

[flightgear.git] / src / FDM / JSBSim / FGPiston.cpp

diff --git a/src/FDM/JSBSim/FGPiston.cpp b/src/FDM/JSBSim/FGPiston.cpp
index aa3cef21d6b38e03b44ad8c1692c8a267c7054e9..dde46eea41ac7981339d5174103707fb38575362 100644 (file)
--- a/src/FDM/JSBSim/FGPiston.cpp
+++ b/src/FDM/JSBSim/FGPiston.cpp
@@ -54,7 +54,8 @@ static const char *IdHdr = ID_PISTON;
 CLASS IMPLEMENTATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-FGPiston::FGPiston(FGFDMExec* exec, FGConfigFile* Eng_cfg) : FGEngine(exec),
+FGPiston::FGPiston(FGFDMExec* exec, FGConfigFile* Eng_cfg, int engine_number)
+  : FGEngine(exec, engine_number),
   R_air(287.3),
   rho_fuel(800),                 // estimate
   calorific_value_fuel(47.3e6),
@@ -65,7 +66,6 @@ FGPiston::FGPiston(FGFDMExec* exec, FGConfigFile* Eng_cfg) : FGEngine(exec),
 
   Type = etPiston;
   crank_counter = 0;
-  EngineNumber = 0;
   OilTemp_degK = 298;
   MinManifoldPressure_inHg = 6.5;
   MaxManifoldPressure_inHg = 28.5;