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  1. 1
    Homogeneous boundary layer at an axisymmetric stagnation point with large rates of injection /

    Homogeneous boundary layer at an axisymmetric stagnation point with large rates of injection / by Libby, Paul A.

    Published 1960
    Government Document Book
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  2. 2
    Resistance of a plate in parallel flow at low Reynolds numbers /

    Resistance of a plate in parallel flow at low Reynolds numbers / by Janour, Zbynek

    Published 1951
    Government Document Book
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  3. 3
    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /

    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / by Stallings, Robert L., Lamb, Milton

    Published 1980
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  4. 4
    An experimental investigation of the NACA 63₁-012 airfoil section with leading-edge and midchord suction slots /

    An experimental investigation of the NACA 63₁-012 airfoil section with leading-edge and midchord suction slots / by McCullough, George B.

    Published 1950
    Government Document Book
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  5. 5
    Influence of refraction on the applicability of the Zehnder-Mach interferometer to studes of cooled boundary layers /

    Influence of refraction on the applicability of the Zehnder-Mach interferometer to studes of cooled boundary layers / by Kinsler, Martin R.

    Published 1951
    Government Document Book
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  6. 6
    Examples of three representative types of airfoil-section stall at low speed /

    Examples of three representative types of airfoil-section stall at low speed / by McCullough, George B.

    Published 1951
    Government Document Book
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  7. 7
    Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0 /

    Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0 / by Spahr, J. Richard

    Published 1951
    Government Document Book
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  8. 8
    On reflection of shock waves from boundary layers /

    On reflection of shock waves from boundary layers / by Liepmann, H. W. (Hans Wolfgang), 1914-2009

    Published 1951
    Government Document Book
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  9. 9
    An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow /

    An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow / by Higgins, Robert W.

    Published 1951
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  10. 10
    Theoretical investigation of submerged inlets at low speeds /

    Theoretical investigation of submerged inlets at low speeds / by Sacks, Alvin H.

    Published 1951
    Government Document Book
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  11. 11
    Experimental investigation of localized regions of laminar-boundary-layer separation /

    Experimental investigation of localized regions of laminar-boundary-layer separation / by Bursnall, William J.

    Published 1951
    Government Document Book
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  12. 12
    Vertical profiles of wind speeds from measurements of high towers /

    Vertical profiles of wind speeds from measurements of high towers / by Borisenko, M. M., Zavarina, M. V.

    Published 1968
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  13. 13
    Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds /

    Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds / by Wimbrow, William R.

    Published 1949
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  14. 14
    Three-dimensional compressible laminar boundary-layer flow /

    Three-dimensional compressible laminar boundary-layer flow / by Moore, F. K. (Franklin K.)

    Published 1951
    Government Document Book
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  15. 15
    Investigations relating to the extension of laminar flow by means of boundary-layer suction through slots /

    Investigations relating to the extension of laminar flow by means of boundary-layer suction through slots / by Loftin, Laurence K.

    Published 1949
    Government Document Book
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  16. 16
    Boundary-layer and stalling characteristics of the NACA 64A006 airfoil section /

    Boundary-layer and stalling characteristics of the NACA 64A006 airfoil section / by McCullough, George B.

    Published 1949
    Government Document Book
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  17. 17
    Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities /

    Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities / by Chapman, Dean R.

    Published 1952
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  18. 18
    Attainable circulation of airfoils in cascade /

    Attainable circulation of airfoils in cascade / by Goldstein, Arthur W.

    Published 1949
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  19. 19
    Effects of boundary-layer displacement and leading-edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds /

    Effects of boundary-layer displacement and leading-edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds / by Bertram, Mitchel H.

    Published 1958
    Government Document Book
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  20. 20
    Influence of wall boundary layer upon the performance of an axial-flow fan rotor /

    Influence of wall boundary layer upon the performance of an axial-flow fan rotor / by Boxer, Emanuel

    Published 1951
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