An Approximate Method For The Calculation Of The Reynolds Analogy Factor For A Compressible Turbulent Boundary Layer In A Pressure Gradient

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An Approximate Method for the Calculation of the Reynolds Analogy Factor for a Compressible Turbulent Boundary Layer in a Pressure Gradient
Language: en
Pages: 96
Authors: Neal Tetervin
Categories: Enthalpy
Type: BOOK - Published: 1967 - Publisher:

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The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient.
An Approximate Method for the Calculation of the Reynolds Analogy Factor for a Compressible Turbulent Boundary Layer in a Pressure Gradient
Language: en
Pages: 66
Authors: Neal Tetervin
Categories:
Type: BOOK - Published: 1967 - Publisher:

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The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient.
An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient
Language: en
Pages: 104
Authors: David L. Brott
Categories: Compressibility
Type: BOOK - Published: 1969 - Publisher:

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The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where th
NOL Hypervelocity Wind Tunnel
Language: en
Pages: 70
Authors: Naval Ordnance Laboratory (White Oak, Md.).
Categories: Hypersonic wind tunnels
Type: BOOK - Published: 1971 - Publisher:

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Technical Abstract Bulletin
Language: en
Pages: 850
Authors:
Categories: Science
Type: BOOK - Published: - Publisher:

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