Experimental Investigation of Compressible Boundary Layers Under the Influence of Pressure Gradients
Language: en
Pages: 149
Authors: Raymond C. Wier
Categories: Compressibility
Type: BOOK - Published: 1996-12-01 - Publisher:

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This study examined the effect of mild pressure gradients on the mean and turbulent flow of high-speed boundary layers. Three Mach numbers (1.7, 3.0 and 5.0) we
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
An Experimental Investigation of a Compressible Turbulent Boundary Layer Subjected to a Systematic Variation of Adverse Pressure Gradients
Language: en
Pages: 232
Experimental Investigation of the Effect of a Systematically Varied Adverse Pressure Gradient on the Growth of Turbulent Boundary Layers
Language: en
Pages:
Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers
Language: en
Pages: 124
Authors: David F. Gates
Categories: Supersonic nozzles
Type: BOOK - Published: 1973 - Publisher:

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The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of exper