Results of flight tests on low-wing monoplane; leading-edge slots over entire wing and flaps extending to ailerons increase lift 94 per cent, increase glide angle 4.2 deg.; span, 35 ft.; weight 1800 lb.; 16.3 lb. per hp.; 9.1 lb. per sq. ft. Warner Scarab, 110 hp. at 1850 r.p.m.


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    Title :

    Effect of slots and flaps on lift and drag of McDonnell airplane as determined in flight


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Notes


    Contributors:
    Soule, H.A. (author)


    Publication date :

    1931


    Size :

    12 pages


    Remarks:

    15 Figs., Supp. plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English