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Numerical Study of Turbulent Separation Bubbles with Varying Pressure Gradient and Reynolds Number A family of cases each containing a small separation bubble is treated by direct numerical simulation (DNS), varying two parameters: the severity of the pressure gradients, generated by suction and blowing across the opposite boundary, and the Reynolds number. Each flow contains a well-developed entry region with essentially zero pressure gradient, and all are adjusted to have the same value for the momentum thickness, extrapolated from the entry region to the centre of the separation bubble. Combined with fully defined boundary conditions this will make comparisons with other simulations and turbulence models rigorous; we present results for a set of eight Reynolds-averaged Navier–Stokes turbulence models. Even though the largest Reynolds number is approximately 5.5 times higher than in a similar DNS study we presented in 1997, the models have difficulties matching the DNS skin friction very closely even in the zero pressure gradient, which complicates their assessment. In the rest of the domain, the separation location per se is not particularly difficult to predict, and the most definite disagreement between DNS and models is near reattachment. Curiously, the better models tend to cluster together in their predictions of pressure and skin friction even when they deviate from the DNS, although their eddy-viscosity levels are widely different in the outer region near the bubble (or they do not rely on an eddy viscosity). Stratford’s square-root law is satisfied by the velocity profiles, both at separation and reattachment. The Reynolds-number range covers a factor of two, with the Reynolds number based on the extrapolated momentum thickness equal to approximately 1500 and 3000. This allows tentative estimates of the improvements that even higher values will bring to the model comparisons. The solutions are used to assess models through pressure, skin friction and other measures; the flow fields are also used to produce effective eddy-viscosity targets for the models, thus guiding turbulence-modelling work in each region of the flow.
Document ID
20190026476
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Coleman, G. N. ORCID
(NASA Langley Research Center Hampton, VA, United States)
Rumsey, C. L.
(NASA Langley Research Center Hampton, VA, United States)
Spalart, P. R. ORCID
(Boeing Company Charleston, SC, United States)
Date Acquired
June 18, 2019
Publication Date
May 17, 2018
Publication Information
Publication: Journal of Fluid Mechanics
Publisher: Cambridge University Press
Volume: 847
ISSN: 0022-1120
e-ISSN: 1469-7645
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-28495
Funding Number(s)
PROJECT: ARMD_109492
WBS: 109492.02.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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