4.7 Article

One-point statistics for turbulent wall-bounded flows at Reynolds numbers up to δ+ ≈ 2000

期刊

PHYSICS OF FLUIDS
卷 25, 期 10, 页码 -

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AMER INST PHYSICS
DOI: 10.1063/1.4823831

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资金

  1. Spanish CICYT [TRA2009-11498]
  2. European Research Council [ERC-2010.AdG-20100224]
  3. Office of Science of the U.S. Department of Energy [DE-AC02-06CH11357]
  4. Universidad Politecnica de Madrid

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One-point statistics are presented for new direct simulations of the zero-pressure-gradient turbulent boundary layer in the range Re-theta = 2780-6680, matching channels and pipes at delta(+) approximate to 1000-2000. For tripped boundary layers, it is found that the eddy-turnover length is a better criterion than the Reynolds number for the recovery of the largest flow scales after an artificial inflow. Beyond that limit, the integral parameters, mean velocities, Reynolds stresses, and pressure fluctuations of the new simulations agree very well with the available numerical and experimental data, but show clear differences with internal flows when expressed in wall units at the same wall distance and Reynolds number. Those differences are largest in the outer layer, independent of the Reynolds number, and apply to the three velocity components. The logarithmic increase with the Reynolds number of the maximum of the streamwise velocity and pressure fluctuations is confirmed to apply to experimental and numerical internal and external flows. The new simulations also extend to a wider range of Reynolds numbers, and to more than a decade in wall distance, the evidence for logarithmic intensity profiles of the spanwise velocity and of the pressure intensities. Streamwise velocity fluctuations appear to require higher Reynolds numbers to develop a clear logarithmic profile, but it is argued that the comparison of the available near-wall data with fluctuation profiles experimentally obtained by other groups at higher Reynolds numbers can only be explained by assuming the existence of a mesolayer for the fluctuations. The statistics of the new simulation are available in our website. (C) 2013 AIP Publishing LLC.

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