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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    Titel :

    On nonlinear approach to aeroelastic stability theory


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Kuessner, H.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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