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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    Title :

    Torsion in box wings


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Contributors:


    Publication date :

    1931


    Size :

    44 pages


    Remarks:

    3 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    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