Heat transfer in rough-wall turbulent thermal convection in the ultimate regime

被引:18
|
作者
MacDonald, Michael [1 ,5 ]
Hutchins, Nicholas [1 ]
Lohse, Detlef [2 ,3 ,4 ]
Chung, Daniel [1 ]
机构
[1] Univ Melbourne, Dept Mech Engn, Melbourne, Vic 3010, Australia
[2] Univ Twente, Phys Fluids Grp, MESA Inst, JM Burgers Ctr Fluid Dynam, POB 217, NL-7500 AE Enschede, Netherlands
[3] Univ Twente, Max Planck Ctr Twente, POB 217, NL-7500 AE Enschede, Netherlands
[4] Max Planck Inst Dynam & Self Org, D-37077 Gottingen, Germany
[5] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
来源
PHYSICAL REVIEW FLUIDS | 2019年 / 4卷 / 07期
基金
澳大利亚研究理事会;
关键词
DIRECT NUMERICAL-SIMULATION; RAYLEIGH-BENARD CONVECTION; SURFACE-ROUGHNESS; PRANDTL NUMBER; CHANNEL FLOW; REYNOLDS; TRANSPORT; TEMPERATURE; PROFILES; PLATES;
D O I
10.1103/PhysRevFluids.4.071501
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
Heat and momentum transfer in wall-bounded turbulent flow, coupled with the effects of wall roughness, is one of the outstanding questions in turbulence research. In the standard Rayleigh-Benard problem for natural thermal convection, it is notoriously difficult to reach the so-called ultimate regime in which the near-wall boundary layers are turbulent. Following the analyses proposed by Kraichnan [Phys. Fluids 5, 1374 (1962)] and Grossmann and Lohse [Phys. Fluids 23, 045108 (2011)], we instead utilize recent direct numerical simulations of forced convection over a rough wall in a minimal channel [MacDonald et al., J. Fluid Mech. 861, 138 (2019)] to directly study these turbulent boundary layers. We focus on the heat transport (in dimensionless form, the Nusselt number Nu) or equivalently the heat transfer coefficient (the Stanton number C-h). Extending the analyses of Kraichnan and Grossmann and Lohse, we assume logarithmic temperature profiles with a roughness-induced shift to predict an effective scaling of Nu similar to Ra-0(.)42, where Ra , is the dimensionless temperature difference, corresponding to C-h similar to Re-0.16 where Re is the centerline Reynolds number. This is pronouncedly different from the skin-friction coefficient C-f, which in the fully rough turbulent regime is independent of Re, due to the dominant pressure drag. In rough-wall turbulence, the absence of the analog to pressure drag in the temperature advection equation is the origin for the very different scaling properties of the heat transfer as compared to the momentum transfer. This analysis suggests that, unlike momentum transfer, the asymptotic ultimate regime, where Nu similar to Ra-1/2, will never be reached for heat transfer at finite Rayleigh number.
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页数:11
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