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Theoretical boundaries and internal characteristics of exhaust plumes from three different supersonic nozzlesExhaust plume boundaries and internal characteristics in rocket exhaust plumes calculated for three different supersonic nozzles
Document ID
19650009676
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Andrews, E. H., Jr. (NASA Langley Research Center Hampton, VA, United States)
Craidon, C. B. (NASA Langley Research Center Hampton, VA, United States)
Vick, A. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-2650
Report Number: NASA-TN-D-2650
Accession Number
65N19277
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET EXHAUST
EXHAUST NOZZLE
SUPERSONIC NOZZLE
JET PLUME
ROCKET NOZZLE

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