- inline float GetVcalibratedFPS(void) { return vcas; }
- inline float GetVcalibratedKTS(void) { return vcas*FPSTOKTS; }
- inline float GetVequivalentFPS(void) { return veas; }
- inline float GetVequivalentKTS(void) { return veas*FPSTOKTS; }
+ inline double GetVcalibratedFPS(void) const { return vcas; }
+ inline double GetVcalibratedKTS(void) const { return vcas*fpstokts; }
+ inline double GetVequivalentFPS(void) const { return veas; }
+ inline double GetVequivalentKTS(void) const { return veas*fpstokts; }
+ 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; }