By means of suggested method of structural calculation it is possible rapidly to obtain comparative results due to variations of geometrical proportions of cantilever wings; method useful for exploring possibilities of various wing forms in initial stages of new design; weight of wing spar obtained represents minimum weight attainable under ideal conditions of uniform stress throughout material, and use of wing section having stationary center of pressure. (Aircraft Engr. Supp.)


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    Titel :

    Cantilever wings


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Duncanson, F. (Autor:in)

    Erschienen in:

    Flight ; 21 , n 13


    Erscheinungsdatum :

    1929


    Format / Umfang :

    4 pages


    Anmerkungen:

    9 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Cantilever wings

    Duncanson, F. | Engineering Index Backfile | 1929


    Semi-Cantilever Wings

    Pasqualini, C. / Biro, D. | Emerald Group Publishing | 1935


    Semi-cantilever wings

    Pasqualini, C. / Biro, D. | Engineering Index Backfile | 1935


    Vibrations in cantilever wings

    Rauscher, M. | Engineering Index Backfile | 1929


    Two-spar cantilever wings

    Walker, B.B. | Engineering Index Backfile | 1936