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Contact-surface tailoring in real shock tubesContact surface tailoring of reflected shock wave interaction with boundary layer in real shock tubes
Document ID
19650025800
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Belles, F. E. (NASA Lewis Research Center Cleveland, OH, United States)
Brabbs, T. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3043
Report Number: NASA-TN-D-3043
Accession Number
65N35401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK WAVE INTERACTION
REFLECTED WAVE
SHOCK TUNNEL
BOUNDARY LAYER

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