Lift, drag, and pitching moments were measured for wing with three different sizes of flap; it was found that any gap between flap and wing reduced lift, drag, and pitching moments, but that center-of-pressure movement and ratio of lift were little affected.


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    Titel :

    Wind-tunnel tests of clark Y wing having split flaps with gaps


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1938


    Format / Umfang :

    4 pages


    Anmerkungen:

    3 Supp plates, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :