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FLOW SEPARATION IN A CONTOUR NOZZLE
Document ID
19630000836
Acquisition Source
Jet Propulsion Laboratory
Document Type
Reprint (Version printed in journal)
Authors
E. J. Roschke (Jet Propulsion Lab La Cañada Flintridge, California, United States)
P. F. Massier (Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
August 1, 2013
Publication Date
October 1, 1962
Publication Information
Publication: American Rocket Society Journal
Publisher: American Rocket Society
Volume: 32
Issue: 10
Issue Publication Date: October 1, 1962
DOI: 10.2514/8.6342
Subject Category
Facilities, Research, And Support
Report/Patent Number
JPL-TR-32-317
Report Number: JPL-TR-32-317
Accession Number
63N10710
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ROCKET EXHAUST
CONTOUR
ROCKET NOZZLE
FLOW SEPARATION
NOZZLE
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