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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    Title :

    Simplified method of elastic-stability analysis for thin cylindrical shells


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1947


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English