Description of method by means of which, through simple layouts and calculations, mutual action of spars can be computed in functions of elasticity of different elements; these forces being known, it is very easy to establish more accurate calculation of spars and rationally determine stiffness that cross members should possess; analysis of torsion in wing of thick airfoil is necessary in order to make rational distribution of material between spars; practical calculations given.


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    Title :

    Analysis of torsional stresses in airplane wings


    Additional title:

    Aviation Eng


    Contributors:

    Published in:

    Publication date :

    1929


    Remarks:

    9 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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    WITMER WARNER H | European Patent Office | 2019

    Free access