which is far too warm at altitude. Thus, air density (and aircraft
performance) was too low for a given altitude.
// cout << "YASIM: ground = " << ground << endl;
float pressure = fgGetDouble("/environment/pressure-inhg") * INHG2PA;
- float temp = fgGetDouble("/environment/temperature-degC") + 273.15;
+ float temp = fgGetDouble("/environment/temperature-degc") + 273.15;
// Convert and set:
Model* model = _fdm->getAirplane()->getModel();