Problem solved is that of initially curved circumferential skin strip, representing section of panel midway between frames, continuous over stringers which act as sinking supports and transfer part of internal pressure load to frames; remainder of pressure load produces hoop tension in skin strip, but maximum total stress including bending in skin at stringer, which is evaluated, is usually greater than would arise from hoop tension alone, in unstiffened shell.


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    Title :

    Stress in curved skin panel of pressurized fuselage


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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