Different causes for structural nonlinearities on aircraft; representation of nonlinear force deflection diagrams of aircraft parts by complex Fourier analysis; approximate method for solution of nonlinear flutter equations is developed using systems of homogeneous linear equations; special case of harmonic balance is compared with more accurate solutions. (Received Sept 1960)


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    Title :

    On nonlinear approach to aeroelastic stability theory


    Additional title:

    AGARD -- Report


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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