NUMERICAL STUDY OF CONJUGATE HEAT TRANSFER IN PIN-FIN CHANNELS BASED ON LARGE-EDDY SIMULATION DATA

被引:0
|
作者
Oda, Yutaka [1 ]
Takeishi, Kenichiro [1 ]
Miyake, Yoshiaki [2 ]
机构
[1] Osaka Univ, Dept Mech Engn, 2-1,Yamadaoka, Suita, Osaka 5650871, Japan
[2] Mitsubishi Heavy Ind Co Ltd, Aerosp Syst, Guidance & Prop Div, Komaki, Aichi 4858561, Japan
来源
COMPUTATIONAL THERMAL SCIENCES | 2012年 / 4卷 / 03期
关键词
turbulence; convective heat transfer; RANS; thermal design; heat conduction;
D O I
10.1615/ComputThermalScien.2012004766
中图分类号
O414.1 [热力学];
学科分类号
摘要
Precedent mass transfer experiments and the corresponding large-eddy simulation (LES) by Oda et al. (Proc. 14th Intl. Heat Transfer Conf., IHTC14-23191, Washington, D.C., USA, Aug. 8-13, 2010) and Takeishi et al. (ASME Paper GT2012-69625, 2012) revealed that an inclined pin-fin channel with a wavy endwall shows better "endwall" heat transfer than that with a flat endwall with less or comparable pressure loss, as long as the pin-fin surface was treated as thermally adiabatic. Therefore, in this study, a conjugate heat transfer problem in the pin-fin channels was solved numerically to evaluate the overall heat transfer performance including heat transfer from the pin-fin surface. To this end, an LES-based conjugate heat transfer analysis was newly proposed, which utilizes time-mean velocity and turbulent statistics obtained by preliminary LES to estimate the eddy thermal diffusivity for thermal Reynolds-averaged NavierStokes (RANS) analysis to solve the conjugate heat transfer problem. This method has an advantage over conventional RANS-based methods when the time-mean flow field is difficult to predict due to the complex turbulent flows, e.g., massively separated flows in pin-fin channels. By applying the method to the inclined pin-fin channel with a flat or wavy endwall, it is clarified that the wavy endwall shows a clearly better overall heat transfer rate than the flat endwall when the Biot number is of the order of 10(-1), which represents a typical condition to cool combustor liners of jet engines.
引用
收藏
页码:271 / 282
页数:12
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