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Possible occurrence of boundary shock wavesPossible occurvence of boundary shock waves
Document ID
19660005101
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Martin, E. D. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3195
Report Number: NASA-TN-D-3195
Accession Number
66N14390
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK WAVE PROPAGATION
ATMOSPHERIC ENTRY
BOUNDARY LAYER FLOW
HEAT TRANSFER
ABLATION

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