+ inline double GetMachU(void) const { return machU; }
+
+ inline double GetTotalTemperature(void) const { return tat; }
+ inline double GetTAT_C(void) const { return tatc; }
+
+ // total pressure above is freestream total pressure for subsonic only
+ // for supersonic it is the 1D total pressure behind a normal shock
+ inline double GetTotalPressure(void) const { return pt; }