Because skin of airplane in flight is subjected to combination of stress, attention is given to problem of plate buckling when more than one stress is acting. (Originally issued as Advance Restricted Report L6A05a Mar 1946)


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    Title :

    Critical combinations of longitudinal and transverse direct stress for infinitely long flat plate with edges elastically restrained against rotation


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:
    Batdorf, S.B. (author) / Stein, M. (author) / Libove, C. (author)


    Publication date :

    1947


    Size :

    14 pages


    Remarks:

    6 Supplementary plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :