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TECHNICAL PAPERS

Recent Progress on MILES for High Reynolds Number Flows

[+] Author and Article Information
F. F. Grinstein

Naval Research Laboratory, Laboratory for Computational Physics and Fluid Dynamics, Code 6410, Washington, DC 20375-5344

C. Fureby

The Swedish Defence Research Agency, FOI, Department of Weapons and Protection, Warheads and Propulsion, SE-172 90, Stockholm, Sweden

J. Fluids Eng 124(4), 848-861 (Dec 04, 2002) (14 pages) doi:10.1115/1.1516576 History: Received March 11, 2002; Revised April 22, 2002; Online December 04, 2002
Copyright © 2002 by ASME
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Author please insert Ref. 76
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Figures

Grahic Jump Location
First and second-order statistical moments of the streamwise velocity component, 〈v̄〉x and v̄rmsx, respectively. Panels (a) to (c) show 〈v̄〉x at x/h=1.0, 2.0, and 3.0, respectively, whereas panels (d) to (f ) show v̄rmsx at x/h=1.0, 2.0, and 3.0, respectively. Legend: (○) experiments, 86, (–) MILES+WM, ([[dashed_line]]) OEEVM+WM and ([[dot_dash_line]]) OEEVM. Red (darker) lines represent simulations using the top-hat inlet velocity profile, whereas blue (lighter) lines represent simulations using the flattened parabolic inlet velocity profile.
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Time-averaged (or mean) velocity profiles 〈v̄1〉 normalized by the friction velocity uτ versus the wall-normal distance at Reτ=395 (blue), Reτ=2030 (green), and Reτ=10,000 (red) for all channel flow cases reported in Table 1. Panel (a) represents outer scaling whereas panel (b) represents inner scaling.
Grahic Jump Location
Turbulent kinetic energy v̄1rms, normalized by the friction velocity uτ versus the wall-normal distance at Reτ=395 (blue), Reτ=2030 (green), and Reτ=10,000 (red) for all cases reported in Table 1; outer scaling is used at the horizontal axis
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Resolved Reynolds stress profiles 〈v1v2〉, normalized by the friction velocity uτ versus the wall-normal distance at Reτ=395 (blue), Reτ=2030 (green), and Reτ=10,000 (red) for all cases reported in Table 1; outer scaling is used at the horizontal axis
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Schematic of the Pitz-Daily backward-facing step configuration
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TVD regions for first and second accurate TVD schemes together with selected limiters
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Time-averaged (or mean) velocity profiles 〈v̄1〉 normalized by the friction velocity uτt for fully developed turbulent channel flow at Ret=395 from MILES using different flux-limiters
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Flow visualizations of vortex-ring bifurcation phenomena for AR=4 jets; (a) elliptic cold jets (laboratory), 53 and (b) rectangular cold jets (MILES), 50. The flow direction is from bottom to top and time-sequences progress from left to right, in the numerical visualizations (based on isosurfaces of the vorticity magnitude); (c) sensitivity of vortex ring dynamics to jet initial conditions (Tj/Ta=1 in “cold” case, and Tj/Ta=5 in “hot” case); Re=Γ>90,000, and M=0.6, based on the circulation Γ of the initial vortex rings and transient jet velocity.
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Near-field MILES simulations of vortex-ring dynamics and associated sound generation in free jets emerging from rectangular nozzles, 51; instantaneous visualizations: (a) unforced supersonic jet with AR=2, (b) axially forced subsonic jet with AR=4
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Visualization of the flowfield for the nonreacting case using contours of the instantaneous streamwise velocity component at the centerplane and iso-surfaces of the second invariant, Q, of the velocity gradient tensor
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Contours of streamwise vorticity projected onto the side and bottom walls, vortex lines and iso-surfaces for Q=1 for (a) MILES+WM at 603 resolution at Reτ=2030 and (b) OEEVM+WM at 903 resolution at Reτ=2030

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