Set of equations based on first mode of wing bending; representation of airplane is such that aerodynamic damping of vibratory motion of wing is separate from that of vertical motion of airplane as whole; easily evaluated solution of equations for unit jump forcing function is also presented which may be built up to determine response to any forcing function.


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    Titel :

    Improved method for calculating dynamic response of flexible airplanes to gusts


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Putnam, A.A. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    13 pages


    Anmerkungen:

    9 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :