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      Prandtl and Rayleigh number dependence of heat transport in high Rayleigh number thermal convection

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          Abstract

          Results from direct numerical simulation for three-dimensional Rayleigh-B\'enard convection in samples of aspect ratio Γ=0.23 and Γ=0.5 up to Rayleigh number Ra=2×1012 are presented. The broad range of Prandtl numbers 0.5<Pr<10 is considered. In contrast to some experiments, we do not see any increase in Nu/Ra1/3, neither due to Pr number effects, nor due to a constant heat flux boundary condition at the bottom plate instead of constant temperature boundary conditions. Even at these very high Ra, both the thermal and kinetic boundary layer thicknesses obey Prandtl-Blasius scaling.

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          Large scale dynamics in turbulent Rayleigh-Benard convection

          The progress in our understanding of several aspects of turbulent Rayleigh-Benard convection is reviewed. The focus is on the question of how the Nusselt number and the Reynolds number depend on the Rayleigh number Ra and the Prandtl number Pr, and on how the thicknesses of the thermal and the kinetic boundary layers scale with Ra and Pr. Non-Oberbeck-Boussinesq effects and the dynamics of the large-scale convection-roll are addressed as well. The review ends with a list of challenges for future research on the turbulent Rayleigh-Benard system.
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            Prandtl and Rayleigh number dependence of the Reynolds number in turbulent thermal convection

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              Boundary layer structure in turbulent thermal convection and its consequences for the required numerical resolution

              Results on the Prandtl-Blasius type kinetic and thermal boundary layer thicknesses in turbulent Rayleigh-B\'enard convection in a broad range of Prandtl numbers are presented. By solving the laminar Prandtl-Blasius boundary layer equations, we calculate the ratio of the thermal and kinetic boundary layer thicknesses, which depends on the Prandtl number Pr only. It is approximated as 0.588Pr1/2 for PrPr and as 0.982Pr1/3 for PrPr, with Pr=0.046. Comparison of the Prandtl--Blasius velocity boundary layer thickness with that evaluated in the direct numerical simulations by Stevens, Verzicco, and Lohse (J. Fluid Mech. 643, 495 (2010)) gives very good agreement. Based on the Prandtl--Blasius type considerations, we derive a lower-bound estimate for the minimum number of the computational mesh nodes, required to conduct accurate numerical simulations of moderately high (boundary layer dominated) turbulent Rayleigh-B\'enard convection, in the thermal and kinetic boundary layers close to bottom and top plates. It is shown that the number of required nodes within each boundary layer depends on Nu and Pr and grows with the Rayleigh number Ra not slower than \Ra0.15. This estimate agrees excellently with empirical results, which were based on the convergence of the Nusselt number in numerical simulations.
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                Author and article information

                Journal
                11 February 2011
                2011-05-01
                Article
                10.1017/jfm.2011.354
                1102.2307
                eb3f6873-72ef-4fdf-97a6-bedd2e93290a

                http://arxiv.org/licenses/nonexclusive-distrib/1.0/

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                Custom metadata
                J. Fluid Mech. 688, 31-43 (2011)
                9 pages, 7 figures
                physics.flu-dyn

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