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SSME main combustion chamber and nozzle flowfield analysisAn investigation is presented of the computational fluid dynamics (CFD) tools which would accurately analyze main combustion chamber and nozzle flow. The importance of combustion phenomena and local variations in mixture ratio are fully appreciated; however, the computational aspects of the gas dynamics involved were the sole issues addressed. The CFD analyses made are first compared with conventional nozzle analyses to determine the accuracy for steady flows, and then transient analyses are discussed.
Document ID
19860022182
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Farmer, R. C.
(Continuum, Inc. Huntsville, AL, United States)
Wang, T. S.
(Continuum, Inc. Huntsville, AL, United States)
Smith, S. D.
(Continuum, Inc. Huntsville, AL, United States)
Prozan, R. J.
(Continuum, Inc. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:178893
NASA-CR-178893
CI-FR-0085
Report Number: NAS 1.26:178893
Report Number: NASA-CR-178893
Report Number: CI-FR-0085
Accession Number
86N31654
Funding Number(s)
CONTRACT_GRANT: NAS8-35510
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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