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Direct numerical simulation of curved turbulent channel flowLow Reynolds number, mildly curved, turbulent channel flow has been simulated numerically without subgrid scale models. A new spectral numerical method developed for this problem was used, and the computations were performed with 2 million degrees of freedom. A variety of statistical and structural information has been extracted from the computed flow fields. These include mean velocity, turbulence stresses, velocity skewness, and flatness factors, space time correlations and spectra, all the terms in the Reynolds stress balance equations, and contour and vector plots of instantaneous velocity fields. The effects of curvature on this flow were determined by comparing the concave and convex sides of the channel. The observed effects are consistent with experimental observations for mild curvature. The most significant difference in the turbulence statistics between the concave and convex sides was in the Reynolds shear stress. This was accompanied by significant differences in the terms of the Reynolds shear stress balance equations. In addition, it was found that stationary Taylor-Gortler vortices were present and that they had a significant effect on the flow by contributing to the mean Reynolds shear stress, and by affecting the underlying turbulence.
Document ID
19850003008
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moser, R. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Moin, P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:85974
NASA-TM-85974
REPT-85024
Report Number: NAS 1.15:85974
Report Number: NASA-TM-85974
Report Number: REPT-85024
Accession Number
85N11316
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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