Direct simulation of conjugate heat transfer of jet in channel crossflow

被引:27
作者
Wu, Zhao [1 ]
Laurence, Dominique [1 ]
Iacovides, Hector [1 ]
Afgan, Imran [1 ]
机构
[1] Univ Manchester, Modelling & Simulat Ctr, Sch Mech Aerosp & Civil Engn, Oxford Rd, Manchester M13 9PL, Lancs, England
基金
英国工程与自然科学研究理事会;
关键词
jet in channel crossflow; Conjugate heat transfer; Direct numerical simulation; Low jet-to-crossflow velocity ratio; DIRECT NUMERICAL-SIMULATION; CYCLE THERMAL FATIGUE; STABILITY ANALYSIS; PASSIVE SCALARS; SCHMIDT NUMBER; ROUND JETS; SCHEMES; FIELD;
D O I
10.1016/j.ijheatmasstransfer.2017.03.027
中图分类号
O414.1 [热力学];
学科分类号
摘要
We present a DNS study of a hot, low momentum laminar water jet discharged into a cold turbulent channel stream through a circular orifice in one of the steel channel walls. The channel wall has a finite thickness and its outer side is cooled under Robin type thermal boundary conditions for a realistic external environment, leading to a conjugate heat transfer system. Nusselt number and r.m.s temperature fluctuations on the wall are compared with our earlier DNS results for the simpler iso-thermal and adiabatic conditions at the channel inner surface. Temperature fluctuations inside the channel wall are resolved to provide data for a conjugate heat transfer (CHT) thermal fatigue test case related to the ageing of pipe walls and welds studies, as found, for example, in power plant piping T-junctions. The crossflow Reynolds number is Re = 3333, jet-to-crossflow velocity ratio is R = 1/6 and fluid-to-solid conductivity ratio is 1/64. The near-wall mean flow structures, a horseshoe vortex ahead and on the sides of the jet orifice, a shallow recirculation behind the discharge and a counter-rotating vortex pair drawing in a blanket of cooler cross-flow, lead to a complex convective and turbulent wall heat transfer pattern around the orifice. The main findings are: (i) Wall maps of Nusselt number and r.m.s temperature, for conjugate heat transfer are only qualitatively similar to the iso-thermal and adiabatic wall cases. (ii) Inside the solid 6r.m.e and its dissipation, analysed from RANS modelling perspective, show that predicted thermal spot length scales are discontinuous on the interface, at variance with the 2-point spectrum-derived scales. (iii) At the high wavenumber range, the spanwise temperature spectra decrease according to exponential-decay spectral models for the fluid turbulence in the Kolmogorov range, but with large exponential coefficients increasing with depth inside the solid. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:193 / 208
页数:16
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