This report documents the computer program developed by the Army to evaluate and implement an aerodynamic methodology developed by the Martin Marietta Corporation. The methodology was developed to predict aerodynamic forces on slender missile bodies with low aspect ratio tails at low and high angles of attack, at arbitrary roll angles for both transonic and supersonic velocities. (Author)


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    Title :

    User's Manual for the Martin-Marietta High Angle of Attack Aerodynamic Methodology for Body Tail Missiles


    Contributors:
    G. C. Winn (author)

    Publication date :

    1978


    Size :

    81 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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