FOR the past fifteen years nearly all aircraft structures have been of the shell or stressed-skin type and problems pertaining to this type of structure have been steadily tackled and finally solved for practical use by the designers.


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    Title :

    A Solution to the Problem of Torsion-Flexure


    Subtitle :

    A Method of Using the Principle of Least Work and Calculus of Variations to Establish the Potential Energy Integrals


    Contributors:

    Published in:

    Publication date :

    1950-11-01


    Size :

    3 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Solution to problem of torsion-flexure

    Mordellet, R.L. | Engineering Index Backfile | 1950


    Torsion and flexure

    Gurney, C. | Engineering Index Backfile | 1939


    Torsion and Flexure

    Gurney, C. | Emerald Group Publishing | 1939


    On flexure-torsion flutter criteria

    Simpson, A. | Online Contents | 1999


    Flexure-Torsion Failure of Panels

    Argyris, John H. | Emerald Group Publishing | 1954