Search Results - Von Doenhoff, Albert E.

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  1. 1
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    Determination of general relations for the behavior of turbulent boundary layers / by Von Doenhoff, Albert E.

    Published 1943
    Government Document Book

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  2. 2
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    A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition / by Von Doenhoff, Albert E.

    Published 1956
    Government Document Book

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  3. 3
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    An analysis of the power-off landing maneuver in terms of the capabilities of the pilot and the aerodynamic characteristics of the airplane / by Von Doenhoff, Albert E.

    Published 1953
    Government Document Book

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  4. 4
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    Studies of the use of Freon-12 as a wind-tunnel testing medium / by Von Doenhoff, Albert E.

    Published 1953
    Government Document Book

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  5. 5
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    Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.

    Published 1944
    Government Document Book

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  6. 6
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    A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient / by Von Doenhoff, Albert E.

    Published 1938
    Government Document Book

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  7. 7
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    Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company / by Von Doenhoff, Albert E.

    Published 1944
    Government Document Book

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  8. 8
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    Tests of a 0.1475c aileron with a tab on low-drag section for Curtiss XP-60 airplane in the low-turbulence tunnel / by Von Doenhoff, Albert E.

    Published 1941
    Government Document Book

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  9. 9
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    Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil / by Von Doenhoff, Albert E.

    Published 1942
    Government Document Book

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  10. 10
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    Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence / by Von Doenhoff, Albert E.

    Published 1940
    Government Document Book

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  11. 11
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    An application of the von Ká́rmán-Millikan laminar boundary-layer theory and comparison with experiment / by Von Doenhoff, Albert E.

    Published 1935
    Online Access
    Government Document eBook

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  12. 12
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    A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient / by Von Doenhoff, Albert E.

    Published 1938
    Online Access
    Government Document eBook

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  13. 13
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    A method of rapidly estimating the position of the laminar separation point / by Von Doenhoff, Albert E.

    Published 1938
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    Government Document eBook

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  14. 14
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    An application of the von Kármán-Millikan laminar boundary-layer theory and comparison with experiment / by Von Doenhoff, Albert E.

    Published 1935
    Government Document Book

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  15. 15
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    Note of similarity conditions for flows with heat transfer / by Von Doenhoff, Albert E.

    Published 1948
    Search for the full-text version of this title in HathiTrust
    Government Document Book

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  16. 16
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    A Method of rapidly estimating the position of the laminar separation point / by Von Doenhoff, Albert E.

    Published 1938
    Government Document Book

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  17. 17
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    Low-speed test of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers / by Von Doenhoff, Albert E.

    Published 1947
    Government Document Book

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  18. 18
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    The Langley two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.

    Published 1947
    Government Document Book

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  19. 19
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    Preliminary investigation in the NACA low-turbulence tunnel of low-drag airfoil sections suitable for admitting air at the leading edge / by Von Doenhoff, Albert E.

    Published 1942
    Government Document Book

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  20. 20
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    Theory of wing sections, including a summary of airfoil data / by Abbott, Ira H. A.

    Published 1959
    Other Authors: “…Von Doenhoff, Albert E.…”
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