Method separates aerodynamic and structural calculations, making it possible to use either theoretical or experimental determinations of spanwise loading and to account for induction effects; method can be used to solve usual aerodynamic problems arising in longitudinal and lateral stability and control and to provide structural design criteria.


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    Title :

    Superposition method for calculating aeroelastic behavior of swept wings


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Brown, R.B. (author) / Holtby, K.F. (author) / Martin, H.C. (author)


    Publication date :

    1951


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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