Effect of flap on performance and control of airplane; in wind-tunnel tests, with horizontal tail surfaces removed, flap was found to increase maximum lift coefficient from 1.27 to 2.41; in flight tests, flap was found to decrease minimum speed from 58.8 to 44.4 mph; longitudinal and directional control adversely affected by flap.


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    Titel :

    Full-scale wind-tunnel and flight tests of fair-child 22 airplane equipped with fowler flap


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Beteiligte:
    Dearborn, C.H. (Autor:in) / Soule, H.A. (Autor:in)


    Erscheinungsdatum :

    1936


    Format / Umfang :

    19 pages


    Anmerkungen:

    Bibliography, 25 Supp sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :