Investigation in N.A.C.A. 7 by 10-ft wind tunnel to find increase in maximum lift coefficient obtained by providing model wing with both Fowler trailing-edge extension flap and Handley Page type leading-edge slot; with best combined arrangement max lift coefficient based on original area increased from 3.17, for Fowler wing, to 3.62.


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    Titel :

    Wind-tunnel tests on model wing with fowler flap and specially developed leading-edge clot


    Weitere Titelangaben:

    Nat Advisory-Committee Aeronautics -- Tech Note


    Beteiligte:
    Weick, F.E. (Autor:in) / Platt, R.C. (Autor:in)


    Erscheinungsdatum :

    1933


    Format / Umfang :

    10 pages


    Anmerkungen:

    7 Supp sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Wind-tunnel tests of fowler variable-area wing

    Weick, F.E. / Platt, R.C. | Engineering Index Backfile | 1932


    Wind tunnel tests of the fowler variable area wing

    Weick, Fred E. ;Platt, Robert C. | SLUB | 1932


    The Fowler Wing Flap

    Fowler, Harlan D. | Emerald Group Publishing | 1936


    Wind-tunnel Tests of the Fowler Variable-area Wing

    Weick, Fred E / Platt, Robert C | NTRS | 1932