Tests made in Langley 4.5-ft flutter research tunnel on uniform, untapered model wing by mounting concentrated weights which were 38, 60, 90 and 100% wing weight; wing was mounted as rigid cantilever; moment of inertia, position of chordwise center of gravity of weight, and spanwise location of weight were varied.


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    Titel :

    Experimental investigation of effects of concentrated weights on flutter characteristics of straight cantilever wing


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Runyan, H.L. (Autor:in) / Sewall, J.L. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :