Results of force tests and pressure distribution measurements are presented from wind tunnel investigation to determine effects of size and hinge location of lift and trim flaps on lift and pitching moment characteristics of semi-span tapered wing with 23° sweepback of quarter-chord line.


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    Title :

    Wind-tunnel investigation of split trailing-edge lift and trim flaps on tapered wing with 23° sweepback


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Letko, W. (author) / Feigenbaum, D. (author)


    Publication date :

    1947


    Size :

    13 pages


    Remarks:

    59 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :