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Experimental investigation of the interaction of a plane, oblique, incident-reflecting shock wave with a turbulent boundary layer on a cooled surface. Volume 1 - Test description and data summaryInteraction of plane, oblique, incident reflecting shock wave with turbulent boundary layer on cooled surface - summary
Document ID
19700001377
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kilburg, R. F. (General Dynamics/Fort Worth TX, United States)
Kotansky, D. R. (General Dynamics/Fort Worth TX, United States)
Date Acquired
August 5, 2013
Publication Date
October 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-66841-1-VOL-1
Accession Number
70N10681
Funding Number(s)
CONTRACT_GRANT: NAS1-6588
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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