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Development of a recursion RNG-based turbulence modelReynolds stress closure models based on the recursion renormalization group theory are developed for the prediction of turbulent separated flows. The proposed model uses a finite wavenumber truncation scheme to account for the spectral distribution of energy. In particular, the model incorporates effects of both local and nonlocal interactions. The nonlocal interactions are shown to yield a contribution identical to that from the epsilon-renormalization group (RNG), while the local interactions introduce higher order dispersive effects. A formal analysis of the model is presented and its ability to accurately predict separated flows is analyzed from a combined theoretical and computational stand point. Turbulent flow past a backward facing step is chosen as a test case and the results obtained based on detailed computations demonstrate that the proposed recursion -RNG model with finite cut-off wavenumber can yield very good predictions for the backstep problem.
Document ID
19940009245
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zhou, YE
(NASA Langley Research Center Hampton, VA, United States)
Vahala, George
(NASA Langley Research Center Hampton, VA, United States)
Thangam, S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-93-51
AD-A270206
NAS 1.26:191511
NASA-CR-191511
Report Number: ICASE-93-51
Report Number: AD-A270206
Report Number: NAS 1.26:191511
Report Number: NASA-CR-191511
Accession Number
94N13718
Funding Number(s)
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-19480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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