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Titlebook: Direct and Large-Eddy Simulation IV; Bernard J. Geurts,Rainer Friedrich,Olivier Métais Book 2001 Springer Science+Business Media Dordrecht

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樓主: Flippant
51#
發(fā)表于 2025-3-30 11:42:38 | 只看該作者
Assessment of Some Models for LES without/with Explicit Filtering,er with some models. Of particular interest are models that behave as viscosity at low . and higher order viscosity at high .. The spectral behavior of the models is investigated numerically, in 48. LES of decaying isotropic turbulence (started from 256. DNS). Two diagnostics are used: model dissipation spectrum and obtained energy spectrum.
52#
發(fā)表于 2025-3-30 15:26:15 | 只看該作者
53#
發(fā)表于 2025-3-30 20:29:33 | 只看該作者
54#
發(fā)表于 2025-3-30 21:05:18 | 只看該作者
Springer Handbook of Materials Dataed on the channel width and the mean bulk velocity) by comparing the results to those of physical experiments and previous numerical studies. This comparison shows that with a fourth-order, symmetry-preserving method a 64 × 64 × 32 grid suffices to perform an accurate direct numerical simulation.
55#
發(fā)表于 2025-3-31 01:08:39 | 只看該作者
56#
發(fā)表于 2025-3-31 05:38:21 | 只看該作者
Nondestructive Inspection (NDI)o different Reynolds numbers are conducted. Results for both simulations are in good agreement with filtered DNS data. A significant improvement is shown compared to simulations with no model at the same low resolutions as the LES. The computational cost of the incremental method is similar to that of a Galerkin approximation on the same grid.
57#
發(fā)表于 2025-3-31 11:44:53 | 只看該作者
58#
發(fā)表于 2025-3-31 16:39:37 | 只看該作者
Precision Machinery Using MEMS Technologyoichiometric point, and at the same time, a partially-premixed front propagates along isomixture fraction lines. In two dimensions, this flame growth leads to local edge-flame combustion. The particular role of partially-premixed combustion during this complex ignition process is evidenced from the DNS results
59#
發(fā)表于 2025-3-31 18:49:42 | 只看該作者
60#
發(fā)表于 2025-3-31 23:57:58 | 只看該作者
DNS of Turbulent Supersonic Channel Flow,fects of compressibility are analysed based on the Reynolds stress budgets and comparisons with their incompressible counterparts. DNS data of turbulent supersonic channel flow along permeable walls at . 1.5 and . 3000 are used to analyze in which way wall permeability modifies the turbulence structure of the flow.
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