The wing differential pressure distributions of two vehicles are predicted using FLEXSTAB. Three space shuttle configurations were investigated. Comparisons were made of wind tunnel and analytical data for a selected range of angle of attack, angle of sideslip, and Mach number. A drone-type vehicle was investigated and comparisons were made between flight and analytical data of wing pressure distributions and static longitudinal stability derivatives.


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    Title :

    FLEXSTAB analysis


    Contributors:

    Publication date :

    1976-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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