Technical progress made in each of the disciplinary research areas affecting the design of supersonic cruise aircraft is discussed. The NASA Supersonic Cruise Aircraft Research program has supported an expanded research program in aerodynamics including an ever growing experimental data base, methodology development across the Mach number range, and sonic boom. Progress in the aerodynamics area could facilitate the choice of the highly swept subsonic leading edge, arrow wing, known for superior supersonic cruise efficiency.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Performance Studies for Supersonic Cruise Aircraft


    Contributors:

    Publication date :

    1976-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Aerodynamic design of a Mach 2.2 supersonic cruise aircraft

    RADKEY, R. / WELGE, H. / ROENSCH, R. | AIAA | 1976


    Aerodynamic Design of a Mach 2.2 Supersonic Cruise Aircraft

    R.L. Radkey / H.R. Welge / R.L. Roensch | AIAA | 1978


    III. Supersonic Cruise Aircraft

    Donald D Baals / Cornelius Driver / Owen G Morris | NTRS | 1960