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On the large-eddy simulation of transitional wall-bounded flowsThe structure of the subgrid scale fields in plane channel flow has been studied at various stages of the transition process to turbulence. The residual stress and subgrid scale dissipation calculated using velocity fields generated by direct numerical simulations of the Navier-Stokes equations are significantly different from their counterparts in turbulent flows. The subgrid scale dissipation changes sign over extended areas of the channel, indicating energy flow from the small scales to the large scales. This reversed energy cascade becomes less pronounced at the later stages of transition. Standard residual stress models of the Smagorinsky type are excessively dissipative. Rescaling the model constant improves the prediction of the total (integrated) subgrid scale dissipation, but not that of the local one. Despite the somewhat excessive dissipation of the rescaled Smagorinsky model, the results of a large eddy simulation of transition on a flat-plate boundary layer compare quite well with those of a direct simulation, and require only a small fraction of the computational effort. The inclusion of non-dissipative models, which could lead to further improvements, is proposed.
Document ID
19890019392
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Piomelli, Ugo
(Maryland Univ. College Park., United States)
Zang, Thomas A.
(NASA Langley Research Center Hampton, VA, United States)
Speziale, Charles G.
(NASA Langley Research Center Hampton, VA, United States)
Hussaini, M. Y.
(Institute for Computer Applications in Science and Engineering Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-181883
ICASE-89-55
NAS 1.26:181883
Report Number: NASA-CR-181883
Report Number: ICASE-89-55
Report Number: NAS 1.26:181883
Accession Number
89N28763
Funding Number(s)
PROJECT: RTOP 505-90-21-01
CONTRACT_GRANT: NAS1-18605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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