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. (see also Nat. Advisory Committee for Aeronautics -- Tech. Memorandums, no. 538, Nov. 1929, 14 pp., 8 figs.; and translation in Aerophile, vol. 37, no 17/18, Sept. 1/15, 1929, p. 284, 1 fig)


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    Title :

    Cantilever wings for modern aircraft


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1929


    Size :

    4 pages


    Remarks:

    10 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Cantilever wings for modern aircraft

    Stieger, H.J. | Engineering Index Backfile | 1929


    Cantilever Wings for Modern Aircraft

    Stieger, H.J. | Emerald Group Publishing | 1929


    Cantilever wings for modern aircraft

    Stieger, H.J. | Engineering Index Backfile | 1929


    Cantilever wings

    Duncanson, F. | Engineering Index Backfile | 1929


    Cantilever wings

    Duncanson, F. | Engineering Index Backfile | 1929