1. GARCY,W.: Measurement of aircraft speed, NASA Reference Publication 1046, 1980;
2. RICHIE,V.S.: Several methods for aerodynamic reduction of static pressure sensing errors for aircraft at subsonic, near-sonic, and low supersonic speeds, NASA TR R-18, 1959;
3. LETKO,W.: Investigation of the fuselage interference on a pitot-static tube extending forward from the nose of the fuselage, NASA-TN-1496, 1947;
4. O'BRYAN,T.C., DANFORTH,E.C.B., JOHNSTON,J.F.: Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds, National Advisory Committee for Aeronautics R-1239, 1955;
5. LATIF,A., MASUD,J., SHEIKIH,S.R., PERVEZ,K., QAZI,O.A., QURESHI,H.: Novel aerodynamic compensation pitot-static tube for application in subsonic and supersonic flight regimes, 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006;