THE methods of wing stress analysis at present in use have in most cases been developed on the assumptions that the ribs are rigid in their own planes, and that they may be considered equivalent to an infinite number of infinitely thin ribs, infinitely closely spaced. The problem may then be treated by the methods of the calculus, as was done, for example, in an article by the writer in AIRCRAFT ENGINEERING, January and February, 1943. A more recent and much more comprehensive paper on the same subject has been published by J. Hadji-Argyris and P. C. Dunne in the R. Ac. Society Journal, February, September and November, 1947, and May and June, 1949.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Two-Spar Wing Stress Analysis


    Untertitel :

    A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen


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

    Erschienen in:

    Erscheinungsdatum :

    1949-09-01


    Format / Umfang :

    15 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 | 1943


    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