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Computation of confined coflow jets with three turbulence modelsA numerical study of confined jets in a cylindrical duct is carried out to examine the performance of two recently proposed turbulence models: an RNG-based K-epsilon model and a realizable Reynolds stress algebraic equation model. The former is of the same form as the standard K-epsilon model but has different model coefficients. The latter uses an explicit quadratic stress-strain relationship to model the turbulent stresses and is capable of ensuring the positivity of each turbulent normal stress. The flow considered involves recirculation with unfixed separation and reattachment points and severe adverse pressure gradients, thereby providing a valuable test of the predictive capability of the models for complex flows. Calculations are performed with a finite-volume procedure. Numerical credibility of the solutions is ensured by using second-order accurate differencing schemes and sufficiently fine grids. Calculations with the standard K-epsilon model are also made for comparison. Detailed comparisons with experiments show that the realizable Reynolds stress algebraic equation model consistently works better than does the standard K-epsilon model in capturing the essential flow features, while the RNG-based K-epsilon model does not seem to give improvements over the standard K-epsilon model under the flow conditions considered.
Document ID
19940012406
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zhu, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Shih, T. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:106378
CMOTT-93-14
ICOMP-93-40
NASA-TM-106378
E-8191
AIAA PAPER 93-3120
Report Number: NAS 1.15:106378
Report Number: CMOTT-93-14
Report Number: ICOMP-93-40
Report Number: NASA-TM-106378
Report Number: E-8191
Report Number: AIAA PAPER 93-3120
Meeting Information
Meeting: AIAA Fluid Dynamics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
94N16879
Funding Number(s)
CONTRACT_GRANT: NCC2-233
PROJECT: RTOP 505-90-5K
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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