An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation

An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation
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Total Pages: 72
Release: 1975
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Documentation of Two- and Three-dimensional Hypersonic Shock Wave/turbulent Boundary Layer Interaction Flows
Language: en
Pages: 32
Authors: Marvin I. Kussoy
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1989 - Publisher:

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Documentation of Two- And Three-Dimensional Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows
Language: en
Pages: 28
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-02 - Publisher: Createspace Independent Publishing Platform

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Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer interaction flows at Mach 7 are presented. Test bodies, compose
Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flows
Language: en
Pages:
Authors: C. C. Horstmann
Categories:
Type: BOOK - Published: 1991 - Publisher:

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Experimental Studies of Hypersonic Shock-Wave Boundary-Layer Interactions
Language: en
Pages: 66
Authors: National Aeronautics and Space Adm Nasa
Categories:
Type: BOOK - Published: 2018-11-02 - Publisher:

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Two classes of shock-wave boundary-layer interactions were studied experimentally in a shock tunnel in which a low Reynolds number, turbulent flow at Mach 8 was