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Analysis of liquid rocket engine exhaust plumesLiquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Document ID
19710039164
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Greenwood, T.
Prozan, R.
Ratliff, A.
Seymour, D.
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 70-844
Report Number: AIAA PAPER 70-844
Meeting Information
Meeting: THERMOPHYSICS CONFERENCE
Location: LOS ANGELES, CA
Start Date: June 29, 1970
End Date: July 1, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A19861
Distribution Limits
Public
Copyright
Other

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