Theoretical aerodynamics program TAD predicts aerodynamic characteristics of vehicles with sounding-rocket configurations. These slender, Axisymmetric finned vehicles have a wide range of aeronautical applications from rockets to high-speed armament. TAD calculates characteristics of separate portions of vehicle, calculates interference between portions, and combines results to form total vehicle solution.


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    Title :

    Aerodynamics of Sounding-Rocket Geometries


    Contributors:

    Published in:

    Publication date :

    1982-09-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :





    Rocket aerodynamics

    Krasnov, N. F. ;Koševoj, V. N. | TIBKAT | 1971


    Rocket Aerodynamics

    N. F. Krasnov | NTIS | 1971