Increased use of heavy wing skins, resulting from various aero-structural considerations at high speed, has necessitated more exact plate instability calculations; determination of critical compression stress and effective width of panels that are stiffened by stringer elements fastened along unloaded edges is discussed.


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    Title :

    Effective width of elastically supported flat plates


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Gerard, G. (author)

    Published in:

    Publication date :

    1946


    Size :

    7 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :