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  1. 1
    Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodyamic friction and heat-transfer coefficients /

    Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodyamic friction and heat-transfer coefficients / by Lee, Dorothy B.

    Published 1956
    Government Document Book
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  2. 2
    Experimental investigation of heat transfer through laminar and turbulent boundary layers on a cooled flat plate at a Mach number of 2.4 /

    Experimental investigation of heat transfer through laminar and turbulent boundary layers on a cooled flat plate at a Mach number of 2.4 / by Slack, Ellis G.

    Published 1952
    Government Document Book
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  3. 3
    Experimental investigation of the turbulent-boundary-layer temperature-recovery factor on bodies of revolution at Mach numbers from 2.0 to 3.8 /

    Experimental investigation of the turbulent-boundary-layer temperature-recovery factor on bodies of revolution at Mach numbers from 2.0 to 3.8 / by Stine, Howard A.

    Published 1952
    Government Document Book
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  4. 4
    Preliminary experimental investigation of low-speed turbulent boundary layers in adverse pressure gradients /

    Preliminary experimental investigation of low-speed turbulent boundary layers in adverse pressure gradients / by Sandborn, Virgil A.

    Published 1953
    Government Document Book
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  5. 5
    Analogy between mass and heat transfer with turbulent flow /

    Analogy between mass and heat transfer with turbulent flow / by Callaghan, Edmund E.

    Published 1953
    Government Document Book
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  6. 6
    Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin-friction results /

    Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin-friction results / by Pappas, C. C.

    Published 1954
    Government Document Book
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  7. 7
    An analtyical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer /

    An analtyical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer / by Rubesin, Morris W.

    Published 1954
    Government Document Book
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  8. 8
    Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 /

    Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 / by Beckwith, Ivan E.

    Published 1957
    Government Document Book
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  9. 9
    Free-flight measurements of turbulent-boundary-layer skin friction in the presence of severe aerodynamic heating at Mach numbers from 2.8 to 7.0 /

    Free-flight measurements of turbulent-boundary-layer skin friction in the presence of severe aerodynamic heating at Mach numbers from 2.8 to 7.0 / by Sommer, Simon C.

    Published 1955
    Government Document Book
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  10. 10
    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 /

    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1957
    Government Document Book
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  11. 11
    An experimental study of the turbulent boundary layer on a shock-tube wall /

    An experimental study of the turbulent boundary layer on a shock-tube wall / by Gooderum, Paul B.

    Published 1958
    Government Document Book
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  12. 12
    Analogy between mass and heat transfer with turbulent flow /

    Analogy between mass and heat transfer with turbulent flow / by Callaghan, Edmund E.

    Published 1953
    Online Access
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  13. 13
    Approximate calculation of the compressible turbulent boundary layer with heat transfer and arbitrary pressure gradient /

    Approximate calculation of the compressible turbulent boundary layer with heat transfer and arbitrary pressure gradient / by Reshotko, Eli

    Published 1957
    Government Document Book
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  14. 14
    Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy /

    Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy / by Seiff, Alvin

    Published 1954
    Government Document Book
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