THE effect of axial constraint on box beams of approximately rectangular section, subject to torsion, is of interest to the aircraft designer in connexion with the stressing of two-spar skin-covered wings. The stresses due to torsion in a uniform box with one end built-in have been investigated by D. Williams, both by rigid methods and using the ordinary “engineer's” theory of bending. Three simple types of loading are considered:—


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    Title :

    Torsion in Box Beams


    Subtitle :

    Some Notes on the Effect of End Constraint in Torsion Boxes of Rectangular Section


    Contributors:
    Payne, J.H. (author)


    Publication date :

    1942-01-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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