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Duct flow nonuniformities for Space Shuttle Main Engine (SSME)Analytical capabilities for modeling hot gas flow on the fuel side of the Space Shuttle Main Engines are developed. Emphasis is placed on construction and documentation of a computational grid code for modeling an elliptical two-duct version of the fuel side hot gas manifold. Computational results for flow past a support strut in an annular channel are also presented.
Document ID
19890009996
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
June 30, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HEC-TR-F225968
NASA-CR-183595
NAS 1.26:183595
Report Number: LMSC-HEC-TR-F225968
Report Number: NASA-CR-183595
Report Number: NAS 1.26:183595
Accession Number
89N19367
Funding Number(s)
CONTRACT_GRANT: NAS8-34507
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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