Investigation carried out to determine stress distribution in stiffened conical and orthogonal cylindrical shells cut by planes and subjected to torsional moments; such shells are frequently encountered in aircraft design; for example, cockpit enclosure trays and floors in fuselages, sloping frames and spars in wings; diagrams presented.


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    Title :

    Torsion in conical and cylindrical shells intersected by planes


    Additional title:

    Aircraft Eng


    Contributors:
    David, F.W. (author)

    Published in:

    Publication date :

    1946


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English