FLEXSTAB computer program is used to evaluate trim state, static, and dynamic stability characteristics, inertial and aerodynamic loading, and elastic deformations of aircraft configurations at subsonic and supersonic speeds.


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    Title :

    Stability of an elastic airplane


    Contributors:
    Erickson, L. L. (author) / Polentz, P. P. (author) / Dusto, A. (author) / Hink, G. (author) / Shansen, S. (author)

    Published in:

    Publication date :

    1977-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



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