Method, based on elastic theory for plate buckling and results for 24S-T aluminum alloy Z-stiffened panels, is shown for calculating compressive strength of Z-stiffened panels that develop local instability.


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    Titel :

    Method of calculating compressive strength of Z-stiffened panels that develop local instability


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Gallaher, G.L. (Autor:in) / Boughan, R.B. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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