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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    Titel :

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


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Beteiligte:
    Knight, M. (Autor:in) / Bamber, M.J. (Autor:in)


    Erscheinungsdatum :

    1929


    Format / Umfang :

    13 pages


    Anmerkungen:

    10 Figs. on supp. plates, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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


    The effect of wing tip floating ailerons on the autorotation of a monoplane wing model

    Knight, M. / Wenzinger, C.J. | Engineering Index Backfile | 1930