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Analysis of rocket engine injection combustion processesMixing methodology improvement for the JANNAF DER and CICM injection/combustion analysis computer programs was accomplished. ZOM plane prediction model development was improved for installation into the new standardized DER computer program. An intra-element mixing model developing approach was recommended for gas/liquid coaxial injection elements for possible future incorporation into the CICM computer program.
Document ID
19770012219
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salmon, J. W.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Saltzman, D. H.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1977
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
FR-31531F-2
NASA-CR-150200
Accession Number
77N19163
Funding Number(s)
CONTRACT_GRANT: NAS8-31531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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