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Large-eddy simulation of transitional channel flowA large-eddy simulation (LES) of transition in plane channel flow was carried out. The LES results were compared with those of a fine direct numerical simulation (DNS), and with those of a coarse DNS that uses the same mesh as the LES, but does not use a residual stress model. While at the early stages of transition, LES and coarse DNS give the same results: the presence of the residual stress model was found to be necessary to predict accurately mean velocity and Reynolds stress profiles during the late stages of transition (after the second spike stage). The evolution of single Fourier modes is also predicted more accurately by the LES than by the DNS. As small scales are generated, the dissipative character of the residual stress starts to reproduce correctly the energy cascade. As transition progresses, the flow approaches its fully developed turbulent state, the subgrid scales tend towards equilibrium, and the model becomes more accurate.
Document ID
19910004097
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Piomelli, Ugo
(Maryland Univ. College Park., United States)
Zang, Thomas A.
(NASA Langley Research Center Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AD-A229672
NASA-CR-187465
NAS 1.26:187465
ICASE-90-80
Report Number: AD-A229672
Report Number: NASA-CR-187465
Report Number: NAS 1.26:187465
Report Number: ICASE-90-80
Accession Number
91N13410
Funding Number(s)
CONTRACT_GRANT: NAS1-18605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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