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Measurements Of Shock-Separated Turbulent Boundary LayersReport documents surface and flow-field measurements of two- and three-dimensional, shock-separated, turbulent boundary layers. Data tabulated to facilitate comparison with other measurements and computations. Shows shock-interaction shadowgraph and oil-flow pattern for each angle. Plotted profiles given for pressures, velocities, Reynolds stresses, and turbulent kinetic energies.
Document ID
19900000601
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Brown, J. D. (NASA Ames Research Center, Moffett Field, CA.)
Brown, J. L. (NASA Ames Research Center, Moffett Field, CA.)
Kussoy, M. I. (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
November 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 11
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12298
Accession Number
90B10601
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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