As result of trend toward thicker skin and fewer stiffening elements in aircraft construction larger fraction of load is being carried by skin and thus ability to predict behavior of skin under load has become more important; method of analysis developed to solve these problems. (published 1949, 20¢)


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    Titel :

    Simplified method of elastic-stability analysis for thin cylindrical shells


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Batdorf, S.B. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :