Analysis of box wing by rational methods results in computation of much lower stresses in various members of box than are obtained when present design procedure is followed; method of least work; Burgess' method of load division; membrane analogy method.


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    Titel :

    Torsion in box wings


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Beteiligte:
    Wheatley, J.B. (Autor:in)


    Erscheinungsdatum :

    1931


    Format / Umfang :

    44 pages


    Anmerkungen:

    3 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Torsion in box wings

    Wheatley, John B | NTRS | 1931


    Torsion in box wings

    Wheatley, John B. | SLUB | 1931


    Stressed-Skin Wings in Pure Torsion

    Kittelsen, H.M.J. | Emerald Group Publishing | 1945


    Stresses and deformation in wings subjected to torsion

    Ruffner, B. F. / Hout, Eloise | TIBKAT | 1952


    Stresses and deformations in wings subjected to torsion

    Ruffner, B F / Hout, Eloise | NTRS | 1952