T = 59 - 0.00356 * altitude;
p = 2116 * pow( ((T + 459.7) / 518.6) , 5.256);
- } else if ( 36152 < altitude < 82345 ) { // lower stratosphere
+ } else if ( 36152 < altitude && altitude < 82345 ) { // lower stratosphere
T = -70;
p = 473.1 * pow( e , 1.73 - (0.000048 * altitude) );
inline double get_user_speed() {return user_speed; }
inline int getNum( FGAIBase::object_type ot ) {
- return (0 < ot < FGAIBase::MAX_OBJECTS) ? numObjects[ot] : numObjects[0];
+ return (0 < ot && ot < FGAIBase::MAX_OBJECTS) ? numObjects[ot] : numObjects[0];
}
void processScenario( string filename );