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Performance of a Combustion Driven Shock Tunnel with Application to the Tailored- Interface Operating ConditionsPerformance characteristics of driven tube portion of combustion driven wind tunnel designed for quasi-steady reservoir conditions
Document ID
19660012885
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hiers, R. S. (NASA Ames Research Center Moffett Field, CA, United States)
Loubsky, W. J. (NASA Ames Research Center Moffett Field, CA, United States)
Stewart, D. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1964
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-54960
Report Number: NASA-TM-X-54960
Accession Number
66N22174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK TUNNEL
COMBUSTION WIND TUNNEL
PERFORMANCE CHARACTERISTICS

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