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An analysis of supersonic flow phenomena in conical nozzles by a method of characteristicsMethod of axisymmetric irrotational characteristics used for analyzing supersonic and hypersonic flow of calorically perfect gas through conical nozzles
Document ID
19660024682
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Callis, L. B. (Academia R. P. R. Bucharest, Romania)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3550
Report Number: NASA-TN-D-3550
Accession Number
66N33972
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
PERFECT GAS
SUPERSONIC FLOW
CONICAL NOZZLE

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