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  1. 31
    Wind-tunnel investigation of the effect of power and flaps on the static longitudinal stability and control characteristics of a single-engine high-wing airplane model /
    by Hagerman, John R
    Published 1947

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  2. 32
    Theoretical study of some methods for increasing the smoothness of flight through rough air /
    by Phillips, William H
    Published 1951

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  3. 33
    Estimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepback /
    by Dods, Jules B
    Published 1951

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  4. 34
    Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds /
    by DeYoung, John
    Published 1951

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  5. 35
    An Analytical investigation of effect of high-lift flaps on take-off of light airplanes /
    by Weick, Fred E
    Published 1951

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  6. 36
    Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps /
    by Brewer, Jack D
    Published 1948

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  7. 37
    WInd-tunnel investigation of an NACA 0009 airfoil with 0.25- and 0.50-airfoil-chord plain flaps tested independently an in combination /
    by Spearman, M. Leroy
    Published 1948

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  8. 38
    Systematic airfoil tests in the large wind tunnel of DVL /
    by Doetsch, H
    Published 1938

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  9. 39
    A simple method for increasing the lift of airplane wings by means of flaps /
    by Gruschwitz, E (Eugen)
    Published 1933

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  10. 40
    Six-component measurements on a straight and a 35 degree swept-back trapezoidal wing with and without split flap /
    by Thiel, G
    Published 1947

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