Lift, drag and center of pressure characteristics of model of Fowler variable-area wing measured in N.A.C.A. 7 by 10 ft wind tunnel; highest lift coefficient obtained was 3.17 as compared with 1.27 for main wing alone.


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    Title :

    Wind-tunnel tests of fowler variable-area wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Weick, F.E. (author) / Platt, R.C. (author)


    Publication date :

    1932


    Size :

    6 pages


    Remarks:

    12 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wind-tunnel Tests of the Fowler Variable-area Wing

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


    Wind-tunnel tests of the Fowler variable-area wing

    Weick, Fred E. / Platt, Robert C. | TIBKAT | 1932


    Wind tunnel tests of the fowler variable area wing

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


    The fowler variable area wing

    Fowler, H.D. | Engineering Index Backfile | 1928


    The fowler variable area wing

    Fowler, H.D. | Engineering Index Backfile | 1928