Preliminary tests on model of monoplane wing equipped with wing-tip floating ailerons; lift, drag, and rolling and yawing moments found; rolling moments roughly independent of angle of attack and yawing moments small; with ailerons neutral minimum drag was more than twice that of wing without ailerons; more suitable plan forms and profiles for wing and ailerons would give improved results.


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    Title :

    Wind tunnel tests on a model of a monoplane wing with floating ailerons


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Contributors:
    Knight, M. (author) / Bamber, M.J. (author)


    Publication date :

    1929


    Size :

    13 pages


    Remarks:

    10 Figs. on supp. plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons

    Knight, Montgomery / Bamber, Millard J | NTRS | 1929





    Wind tunnel tests on a model of a monoplane wing with floating allerons

    Knight, Montgomery ;Bamber, Millard J. | SLUB | 1929