Supersonic wind tunnel test of nose-cone angle, upper stage fineness ratio, and transition-flare angle effects on aerodynamic characteristics of simulated launch vehicle


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of configuration geometry on the supersonic aerodynamic characteristics of a simulated launch vehicle


    Contributors:

    Publication date :

    1967-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English