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Improvements in Combustion Smoothness and Efficiency in a Large Shock-tube DriverImprovements in combustion smoothness and efficiency in large shock tube driver
Document ID
19660020075
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Compton, D. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-56498
Report Number: NASA-TM-X-56498
Accession Number
66N29365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMBUSTION EFFICIENCY
SHOCK TUNNEL

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