Distortion of wing under air load causing reduction or reversal of aileron control, weakness in torsion and probability of wing flutter is discussed; increased profile drag; weight; utilization of wing covering for strength; principle of Mono-Spar system; comparison of single and two-spar structures; experimental test wing; wing tip construction. (translation) (See also Aircraft Eng., vol. 1, no. 6, Aug. 1929, pp. 187-190, 10 figs.; Nat. Advisory Committee for Aeronautics -- Tech. Memorandums, no. 538, Nov. 1929, 14 pp., 8 figs.)


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    Title :

    Cantilever wings for modern aircraft


    Additional title:

    Aerophile,


    Contributors:

    Published in:

    Aerophile ; 37 , n 17/18


    Publication date :

    1929


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Cantilever wings for modern aircraft

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