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Analysis of tailored-interface operation of shock tubes with helium-driven planetary gasesAnalysis of tailored interface operation of shock tubes with helium driven planetary gases
Document ID
19660020190
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Loubsky, W. J. (NASA Ames Research Center Moffett Field, CA, United States)
Reller, J. D., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3495
Report Number: NASA-TN-D-3495
Accession Number
66N29480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REAL GAS
SHOCK TUNNEL
COMPUTER METHOD
HELIUM
PERFECT GAS

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