Report is first attempt to devise calculation method for representing buckling behavior of cylindrical shells of variable curvature; problem occurs, for instance, in dimensioning wing noses, stability behavior of which is decisively influenced by variability of curvature. English translation from (ZWB) Forschungsbericht n 1671 Sept 16 1942.


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    Title :

    Stability of cylindrical shell of variable curvature


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1951


    Size :

    64 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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