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

[flightgear.git] / src / FDM / YASim / FGFDM.cpp

diff --git a/src/FDM/YASim/FGFDM.cpp b/src/FDM/YASim/FGFDM.cpp
index cd24f7b7f380a0cb796d90dee732f7274b8c1938..1ebc5247681432a96a2d633fb696f5247dd4fe97 100644 (file)
--- a/src/FDM/YASim/FGFDM.cpp
+++ b/src/FDM/YASim/FGFDM.cpp
@@ -220,6 +220,8 @@ void FGFDM::startElement(const char* name, const XMLAttributes &atts)
        if(a->hasAttribute("epr"))  j->setEPR(attrf(a, "epr"));
        if(a->hasAttribute("exhaust-speed"))
            j->setVMax(attrf(a, "exhaust-speed") * KTS2MPS);
+       if(a->hasAttribute("spool-time"))
+           j->setSpooling(attrf(a, "spool-time"));
        
        j->setPosition(v);
        _airplane.addThruster(j, mass, v);
@@ -529,6 +531,8 @@ void FGFDM::setOutputProperties(float dt)
                 node->setFloatValue("mp-inhg", pe->getMP() * (1/INHG2PA));
                 node->setFloatValue("egt-degf",
                                     pe->getEGT() * K2DEGF + K2DEGFOFFSET);
+                node->setFloatValue("oil-temperature-degf",
+                                    pe->getOilTemp() * K2DEGF + K2DEGFOFFSET);
                 node->setFloatValue("boost-gauge-inhg",
                                     pe->getBoost() * (1/INHG2PA));
             } else if(p->getEngine()->isTurbineEngine()) {