Stability equation for structure acted upon by air forces is set up in form convenient for flutter analysis; unrestricted generalized coordinates in complex form are used; expressions given for aerodynamical coefficients of airfoil in terms of theoretical two-dimensional coefficients; mechanical coefficients for airfoils expressed in terms of quantities generally known or easily calculable; value of empirical data from resonance and static deflection tests emphasized.


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    Titel :

    Three-dimensional flutter analysis


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Bleakney, W.M. (Autor:in)


    Erscheinungsdatum :

    1941


    Format / Umfang :

    8 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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