2009
DOI: 10.1002/fld.2096
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Performance of very‐high‐order upwind schemes for DNS of compressible wall‐turbulence

Abstract: SUMMARYThe purpose of the present paper is to evaluate very-high-order upwind schemes for the direct numerical simulation (DNS) of compressible wall-turbulence. We study upwind-biased (UW) and weighted essentially nonoscillatory (WENO) schemes of increasingly higher order-of-accuracy (J.

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Cited by 27 publications
(49 citation statements)
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References 94 publications
(251 reference statements)
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“…Computed p rms corresponds, for the present dns results (Fig. 8), to the fluctuation of the actual thermodynamic pressure, obtained from the equation-of-state (Gerolymos et al 2010). There is quite good agreement of present results for p rms with the incompressible dns of Kim et al (1987), obtained with similar resolution on the same computational box (Fig.…”
Section: Fluctuating Pressure Fieldsupporting
confidence: 81%
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“…Computed p rms corresponds, for the present dns results (Fig. 8), to the fluctuation of the actual thermodynamic pressure, obtained from the equation-of-state (Gerolymos et al 2010). There is quite good agreement of present results for p rms with the incompressible dns of Kim et al (1987), obtained with similar resolution on the same computational box (Fig.…”
Section: Fluctuating Pressure Fieldsupporting
confidence: 81%
“…For this reason the turbulent correlations obtained can be considered as incompressible. This has been verified by systematic comparison with standard incompressible pseudospectral dns data (Kim et al 1987;Moser et al 1999;delÁlamo & Jiménez 2003;delÁlamo et al 2004;Hoyas & Jiménez 2006, 2008, both for single point statistics (Gerolymos et al 2010, all soms † and toms ‡ appearing in the Reynolds-stress budgets) and for spectra of velocity fluctuations in the homogeneous [Lx, Ly, Lz (Nx, Ny, Nz) are the dimensions (number of grid-points) of the computational domain (x = homogeneous streamwise, y = normal-to-the-wall, z = homogeneous spanwise direction); δ is the channel halfheight; ∆x + , ∆y + w , ∆y + cl , ∆z + are the mesh-sizes in wall-units; (·)w denotes wall and (·)cl centerline values; N y + ≤10 is the number of grid points between the wall and y + = 10; Reτ w :=ūτ δν −1 w ;ūτ is the friction velocity; δ is the channel halfheight;νw = is the kinematic viscosity at the wall;Mcl is the centerline Mach-number; ∆t + is the computational time-step in wall-units; t + obs is the observation period in wall units over which statistics were computed; ∆t + s is the sampling time-step for the single-point statistics in wall-units; ∆t + s R 2 is the sampling time-step for the two-point statistics in wall-units].…”
Section: Plane Channel Flow Configuration and Computational Methodsmentioning
confidence: 57%
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