Search Results - Braslow, Albert L.

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  1. 1
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    Further experimental studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil / by Braslow, Albert L.

    Published 1950
    Government Document Book

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  2. 2
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    Investigation of effects of various camouflage paints and painting procedures onthe drag characteristics of an NACA 65(421)-420, a = 1.0 airfoil section / by Braslow, Albert L.

    Published 1944
    Government Document Book

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  3. 3
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    Investigation of surface irregularities on an NACA 63(420)-416, a = 1.0 airfoil section for the Glenn L. Martin Company design 195 / by Braslow, Albert L.

    Published 1943
    Government Document Book

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  4. 4
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    A history of suction-type laminar-flow control with emphasis on flight research / by Braslow, Albert L.

    Published 1999
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    Government Document eBook

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  5. 5
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    Analysis of boundary-layer transition on X-15-2 research airplane / by Braslow, Albert L.

    Published 1966
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    Government Document Book

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  6. 6
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    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
    Government Document Book

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  7. 7
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    A history of suction-type laminar-flow control with empahsis on flight research / by Braslow, Albert L.

    Published 1999
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    Government Document Book

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  8. 8
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    Investigation of boundary-layer Reynolds number for transition on an NACA 65₍₂₁₅₎-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel / by Braslow, Albert L.

    Published 1948
    Government Document Book

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  9. 9
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    Two-dimensional wind-tunnel investigation of sealed 0.22-airfoil-chord internally balanced ailerons of different contour on an NACA 65(112)-213 airfoil / by Braslow, Albert L.

    Published 1946
    Government Document Book

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  10. 10
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    Two-dimensional wind-tunnel investigation of an approximately 14-percent thick NACA 66-series-type airfoil section with a double slotted flap / by Braslow, Albert L.

    Published 1946
    Government Document Book

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  11. 11
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    Two-dimensional wind-tunnel investigation of low-drag vertical-tail, horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces / by Braslow, Albert L.

    Published 1946
    Government Document Book

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  12. 12
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    Simplified method for determination of critical height of distributed roughness for boundary-layer transition at Mach numbers from 0 to 5 / by Braslow, Albert L.

    Published 1958
    Government Document Book

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  13. 13
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    Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system / by Maddalon, Dal V., Braslow, Albert L.

    Published 1990
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  14. 14
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    Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively / by Patterson, Elizabeth W., Braslow, Albert L.

    Published 1961
    Government Document Book

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  15. 15
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    Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction / by Schwartzberg, Milton A.

    Published 1952
    Other Authors: “…Braslow, Albert L.…”
    Government Document Book

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  16. 16
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    Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively / by Patterson, Elizabeth W.

    Published 1958
    Other Authors: “…Braslow, Albert L.…”
    Government Document Book

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  17. 17
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    Experimental and theoretical studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil / by Burrows, Dale L.

    Published 1949
    Other Authors: “…Braslow, Albert L.…”
    Government Document Book

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  18. 18
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    Studies of the use of Freon-12 as a wind-tunnel testing medium / by Von Doenhoff, Albert E.

    Published 1953
    Other Authors: “…Braslow, Albert L.…”
    Government Document Book

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  19. 19
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    Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(1)-210 airfoil section / by Underwood, William J.

    Published 1945
    Other Authors: “…Braslow, Albert L.…”
    Government Document Book

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  20. 20
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    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Published 1952
    Other Authors: “…Braslow, Albert L.…”
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    Government Document Electronic eBook

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