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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    Titel :

    A Solution to the Problem of Torsion-Flexure


    Untertitel :

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


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.11.1950


    Format / Umfang :

    3 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    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