Sheet in airplane wings, fuselages, and hull bottoms reinforced by stringers frequently is subjected to normal pressure as well as forces in plane of sheet; solution presented for buckling load and load carried after buckling of clamped plate having width-length ratio of 1:4 under combined normal pressure and axial load. See also Engineering Index 1945 p 844.


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    Titel :

    Clamped long rectangular plate under combined axial load and normal pressure


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Woolley, R.M. (Autor:in) / Corrick, J.N. (Autor:in) / Levy, S. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    14 pages


    Anmerkungen:

    Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Clamped long rectangular plate under combined axial load and normal pressure

    Woolley, Ruth M / Corrick, Josephine N / Levy, Samuel | NTRS | 1946


    Clamped long rectangular plate under combined axial load and normal pressure

    Woolley, Ruth M. / Corrick, Josephine N. / Levy, Samuel | TIBKAT | 1945


    Simply supported long rectangular plate under combined axial load and normal pressure

    Levy, Samuel / Goldenberg, Daniel / Zibritosky, George | NTRS | 1944


    Simply supported long rectangular plate under combined axial load and normal pressure

    Levy, Samuel / Goldenberg, Daniel / Zibritosky, George | TIBKAT | 1944