-private:
- float vcas;
- float veas;
- float mach;
- float qbar,rhosl,rho,p,psl,pt;
- //Don't add a getter for pt!
- //pt above is freestream total pressure for subsonic only
- //for supersonic it is the 1D total pressure behind a normal shock
- //if a general freestream total is needed, e-mail Tony Peden
- // (apeden@earthlink.net) or you can add it your self using the
- // isentropic flow equations