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Second order modeling of boundary-free turbulent shear flowsA set of realizable second order models for boundary-free turbulent flows is presented. The constraints on second order models based on the realizability principle are re-examined. The rapid terms in the pressure correlations for both the Reynolds stress and the passive scalar flux equations are constructed to exactly satisfy the joint realizability. All other model terms (return-to-isotropy, third moments, and terms in the dissipation equations) already satisfy realizability. To correct the spreading rate of the axisymmetric jet, an extra term is added to the dissipation equation which accounts for the effect of mean vortex stretching on dissipation. The test flows used in this study are the mixing shear layer, plane jet, axisymmetric jet, and plane wake. The numerical solutions show that the unified model equations predict all these flows reasonably. It is expected that these models would be suitable for more complex and critical flows.
Document ID
19910013211
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Shih, T.-H.
(NASA Lewis Research Center Cleveland, OH., United States)
Chen, Y.-Y.
(Sandia National Labs. Albuquerque, NM., United States)
Lumley, J. L.
(Cornell Univ. Ithaca, NY., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICOMP-91-07
NASA-TM-104369
CMOTT-91-02
E-6170
NAS 1.15:104369
Report Number: ICOMP-91-07
Report Number: NASA-TM-104369
Report Number: CMOTT-91-02
Report Number: E-6170
Report Number: NAS 1.15:104369
Accession Number
91N22524
Funding Number(s)
CONTRACT_GRANT: NASA ORDER C-99066-G
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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