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Jet Effects on Cylindrical Afterbodies Housing Sonic and Supersonic Nozzles which Exhaust Against a Supersonic Stream at Angles of Attack from 90 to 180Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles
Document ID
19620000601
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Hayman, Lovick O., Jr. (NASA Langley Research Center Hampton, VA, United States)
McDearmon, Russell W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
March 1, 1962
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-1016
Report Number: NASA-TN-D-1016
Accession Number
62N10601
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE
SONIC NOZZLE
SUPERSONIC NOZZLE
AFTERBODY
FLUID MECHANICS
CYLINDRICAL AFTERBODY
JET
SHOCK WAVE

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