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Turbulent Recirculating Flows in Isothermal Combustor GeometriesComputer program developed that provides mathematical solution to design and construction of combustion chambers for jet engines. Improved results in areas of combustor flow fields accomplished by this computerprogram solution, cheaper and quicker than experiments involving real systems for models.
Document ID
19840000128
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Lilley, D. (Oklahoma State University)
Rhode, D. (Oklahoma State University)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13894
Accession Number
84B10128
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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