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Jun 2012

Volume 24, Issue 6, Articles (06xxxx)

Issue Cover Spotlight Figure

Phys. Fluids 24, 063302 (2012); http://dx.doi.org/10.1063/1.4729453 (18 pages)

Wenbo Tang, Brent Knutson, Alex Mahalov, and Reneta Dimitrova
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Droplet size distribution in homogeneous isotropic turbulence

Prasad Perlekar, Luca Biferale, Mauro Sbragaglia, Sudhir Srivastava, and Federico Toschi

Phys. Fluids 24, 065101 (2012); http://dx.doi.org/10.1063/1.4719144 (9 pages)

Online Publication Date: 6 June 2012

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We study the physics of droplet breakup in a statistically stationary homogeneous and isotropic turbulent flow by means of high resolution numerical investigations based on the multicomponent lattice Boltzmann method. We verified the validity of the criterion proposed by Hinze [AIChE J. 1, 289 (1955)] for droplet breakup and we measured the full probability distribution function of droplets radii at different Reynolds numbers and for different volume fractions. By means of a Lagrangian tracking we could follow individual droplets along their trajectories, define a local Weber number based on the velocity gradients, and study its cross-correlation with droplet deformation.
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47.55.df Breakup and coalescence
47.27.eb Statistical theories and models
47.27.Gs Isotropic turbulence; homogeneous turbulence
02.50.Cw Probability theory
47.11.Qr Lattice gas

Numerical study of the influence of the Reynolds-number on the lift created by a leading edge vortex

Xiaoqin Zhang and Jörg U. Schlüter

Phys. Fluids 24, 065102 (2012); http://dx.doi.org/10.1063/1.4718322 (8 pages)

Online Publication Date: 13 June 2012

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We present a numerical study on the influence of the Reynolds-number on the lift enhancing effect of a leading edge vortex. Our approach is based on a combination of large-eddy simulations and the immersed boundary technique. We determine the influence of the leading edge vortex on the unsteady lift by simulating a fast pitch-up motion of the plate and studying the lift evolution after holding the flat plate fixed at an angle of attack. Our results suggest that an optimal Reynolds-number exists that maximizes the lift of the leading edge vortex, but that the lift-to-drag ratio is largely independent of the Reynolds-number above a Reynolds-number of Rec > 2000.
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47.32.C- Vortex dynamics
02.60.-x Numerical approximation and analysis
47.11.-j Computational methods in fluid dynamics
47.27.ep Large-eddy simulations

A compressible wall model for large-eddy simulation with application to prediction of aerothermal quantities

S. Bocquet, P. Sagaut, and J. Jouhaud

Phys. Fluids 24, 065103 (2012); http://dx.doi.org/10.1063/1.4729614 (42 pages) | Cited 1 time

Online Publication Date: 26 June 2012

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Large-eddy simulation (LES) of compressible flow with wall modelling is assessed on a quasi-isothermal and supersonic plane channel. The derivation of a quasi-analytical wall model based on empirical laws appears very difficult for combined physical effects like compressibility with pressure gradient. A wall model based on the compressible thin boundary layer equations constitutes a more general approach toward the simulation of multiphysical wall bounded flows with LES. In this work, such a wall model is derived and solved thanks to a new meshless method. An adequate scaling of the wall distance is introduced in the Van-Driest damping function of the wall model to handle compressibility effects. The choice of the proper wall distance scaling is shown to be crucial as soon as compressibility effects become significant. Additionally, some sources of error inherent to this wall-modelling approach are treated by appropriate corrections, and show non-negligible impact on the results. On a quasi-isothermal plane channel flow, the mean wall fluxes, primitive variable profiles and velocity fluctuations compare well to Direct Numerical Simulation (DNS) and empirical correlations for a wide range of Reynolds number. Then the DNS of supersonic isothermal-wall plane channel of Coleman at Mach = 1.5 and Mach = 3 are used as a more discriminant test case. The results agree well with the DNS data in terms of mean wall friction and wall heat flux. Finally, a specific analysis of the wall model accuracy is performed outside of the LES solver. This analysis allows to discriminate the error due to the wall model itself from the error due to the interaction between the wall model and the LES solver.
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47.40.Ki Supersonic and hypersonic flows
47.27.ep Large-eddy simulations
47.27.nb Boundary layer turbulence
47.27.nd Channel flow
47.27.te Turbulent convective heat transfer

A subgrid-scale model for large-eddy simulation based on the physics of interscale energy transfer in turbulence

Brian W. Anderson and J. Andrzej Domaradzki

Phys. Fluids 24, 065104 (2012); http://dx.doi.org/10.1063/1.4729618 (35 pages)

Online Publication Date: 28 June 2012

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The scale-similarity model in large-eddy simulation (LES) leads to an attractive, functionally simple expression for the subgrid-scale (SGS) stress tensor. It is well known, however, that the similarity model fails to accurately predict some of the most fundamental quantities in turbulent flows, perhaps the most important being the global energy transfer and the associated subgrid-scale dissipation. To address this, additional dissipative terms are usually added to the similarity model to improve its performance. In the present paper, considerations of interscale energy transfer have been used to identify sources of the observed deficiencies of the similarity model, specifically its inadequate balancing of terms contributing energy to the smallest scales and its duplication of terms producing effects in the largest scales. These considerations provide guidance in the development of a new model, which shows more favorable characteristics of energy transfer while preserving the functional simplicity of the scale-similarity model. Partial nonlinear terms are used to decompose the nonlinear transfer present in LES and to formulate a model expression capable of balancing small-scale production terms depositing energy near the LES cutoff. The proposed model is formulated in the same vein as the scale-similarity model, consisting of test filtered velocities and their products, but offers clear improvements in predictions of mean flow quantities and the global energy flux from the resolved to subgrid scales without the need for additional terms to augment subgrid-scale energy dissipation. The application of the new interscale transfer model in LES of wall-bounded flows leads to predictions of mean and RMS flow quantities comparable to those obtained for other, established SGS models.
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47.27.nb Boundary layer turbulence
47.11.-j Computational methods in fluid dynamics
47.27.ep Large-eddy simulations
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