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Contract-surface tailoring in real shock tubesEquilibrium pressure measured after interaction of reflected shock with contact surface to determine tailored conditions in real shock tubes
Document ID
19660020169
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
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
January 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-56735
Report Number: NASA-TM-X-56735
Accession Number
66N29459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE MEASUREMENT
GAS DYNAMICS
SHOCK TUNNEL
EQUILIBRIUM

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