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Shock induced boundary layer over a semi-infinite flat plate. Part 1: Flow in the immediate vicinity of the shock waveLaminar, two dimensional boundary layer generated in immediate vicinity of plane shock wave moving over flat plate into gas initially at rest
Document ID
19710028358
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Abbott, D. E. (Purdue Univ. West Lafayette, IN, United States)
Ero, M. I. O. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-123159
FMTR-70-1-PT-1
Report Number: NASA-CR-123159
Report Number: FMTR-70-1-PT-1
Accession Number
71N37834
Funding Number(s)
CONTRACT_GRANT: NGR-15-005-077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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