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Examination of various turbulence models for application in liquid rocket thrust chambersThere is a large variety of turbulence models available. These models include direct numerical simulation, large eddy simulation, Reynolds stress/flux model, zero equation model, one equation model, two equation k-epsilon model, multiple-scale model, etc. Each turbulence model contains different physical assumptions and requirements. The natures of turbulence are randomness, irregularity, diffusivity and dissipation. The capabilities of the turbulence models, including physical strength, weakness, limitations, as well as numerical and computational considerations, are reviewed. Recommendations are made for the potential application of a turbulence model in thrust chamber and performance prediction programs. The full Reynolds stress model is recommended. In a workshop, specifically called for the assessment of turbulence models for applications in liquid rocket thrust chambers, most of the experts present were also in favor of the recommendation of the Reynolds stress model.
Document ID
19930002821
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hung, R. J.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
April 30, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:184406
NASA-CR-184406
Report Number: NAS 1.26:184406
Report Number: NASA-CR-184406
Accession Number
93N12009
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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