This report deals with an investigation carried out in the Civil Engineering Laboratory of the University of California, to determine the accuracy of existing methods of computing the stresses in an airplane fuselage when subjected to torsion, and to derive a simple approximate formula for the rapid calculation of these stresses.


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    Title :

    A Short Method of Calculating Torsional Stresses in an Airplane Fuselage


    Contributors:

    Publication date :

    1924-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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