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A theoretical study of the effect on expansion-tube performance of area changes at primary and secondary diaphragm stationsDivergent nozzle location effects on viscous and diaphragm problems in expansion tube supersonic flow
Document ID
19660009026
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Callis, L. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3303
Accession Number
66N18315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VISCOUS FLOW
EXPANSION
SUPERSONIC FLOW
DIVERGENT NOZZLE
DIAPHRAGM

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