Effect of Tensile Stresses in the Bottom Skin WE now come to the investigation of the effect of tensile stresses in the bottom skin. In this case, the analysis is necessarily more complicated than the preceding, but it will be found that the mathematical work is essentially the same, and that we have the same basic equations simply with more terms in them. In particular, the condition for minimum strain energy is the same as equation (9), but the expressions for X and Y are more complicated. As before, the quantity Y depends only on the structure of the wing, while X depends on both the structure and the applied loads. The quantity Z is the same as before.


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    Titel :

    Two-Spar Wing Stress Analysis


    Untertitel :

    The Mathematical Theory, with Numerical Examples


    Beteiligte:
    Goodey, W.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1943-02-01


    Format / Umfang :

    17 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Two-Spar Wing Stress Analysis

    Goodey, W.J. | Emerald Group Publishing | 1941


    Two-Spar Wing Stress Analysis

    Goodey, W.J. | Emerald Group Publishing | 1944


    Two-spar wing stress analysis

    Goodey, W.J. | Engineering Index Backfile | 1943


    Two-Spar Wing Stress Analysis

    Goodey, W.J. | Emerald Group Publishing | 1943


    Two-Spar Wing Stress Analysis

    Goodey, W.J. | Emerald Group Publishing | 1949