Considers cantilever wing with two spars and similar wing with three spars in approximate computation; author seeks to determine effect of variously loaded spars on one another, since neglect of this effect would present economically very unfavorable computation method.


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    Title :

    Computation of cantilever airplane wings


    Additional title:

    U.S. Nat. Advisory Comm. Aeronautics -- Tech. Memorandums


    Contributors:
    Thalau, I. (author)


    Publication date :

    1925


    Size :

    21 pages


    Remarks:

    15 Figs. on supp. plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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