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
Author :
Publisher :
Total Pages : 72
Release :
ISBN-10 : NASA:31769000530991
ISBN-13 :
Rating : 4/5 (91 Downloads)

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

Download or read book An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation written by and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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

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:

DOWNLOAD EBOOK

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

DOWNLOAD EBOOK

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:

DOWNLOAD EBOOK

Experimental Studies of Hypersonic Shock-Wave Boundary-Layer Interactions
Language: en
Pages: 66
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-06 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

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