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  1. 111
    Wind-tunnel investigation of effect of wing location, power, and flap deflection on effective dihedral of a typical single-engine fighter-airplane model with tail removed /
    by Tucker, Warren A
    Published 1946

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  2. 112
    Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle /
    by Kuhn, Richard E
    Published 1956

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  3. 113
    Resume of air-load data on slats and flaps /
    by Wenzinger, Carl J
    Published 1939

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  4. 114
    Wind-tunnel investigation of the boundary layer and wake and their relation to airfoil characteristics - NACA 65₁-012 airfoil with a true contour flap and a beveled-trailing-edge flap /
    by Mendelsohn, Robert A
    Published 1947

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  5. 115
    Wind-tunnel investigation of the effect of power and flaps on the static longitudinal stability characteristics of a single-engine low-wing airplane model /
    by Wallace, Arthur R
    Published 1947

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  6. 116
    Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab /
    by Braslow, Albert L
    Published 1947

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  7. 117
    The Effect of slots and flaps on the lift and drag of the McDonnell airplane as determined in flight /

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  8. 118
    Wind-tunnel tests of a Hall high-lift wing /
    by Weick, Fred E
    Published 1932

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  9. 119
    Wind tunnel pressure distribution tests on an airfoil with trailing edge flap /
    by Wenzinger, Carl J
    Published 1929

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  10. 120
    Wind tunnel tests on a model of a monoplane wing with floating ailerons /
    by Knight, Montgomery
    Published 1929

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