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首页> 外文期刊>International Journal of Heat and Mass Transfer >Evaluation of a developed SST k-ω turbulence model for the prediction of turbulent slot jet impingement heat transfer
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Evaluation of a developed SST k-ω turbulence model for the prediction of turbulent slot jet impingement heat transfer

机译:湍流槽射流冲击热传递预测开发SST k-Ω湍流模型的评价

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摘要

In this paper, a turbulence model based on OpenFOAM has been developed for the jet impingement heat transfer, which is based on the standard SST k-omega model and considers the effects of cross-diffusion term and the Kato-Launder model. The effects of the modifications have been studied for different nozzle-plate spacing of 4 and 9.2 in terms of pressure distributions, mean velocity, skin friction and the local Nusselt number distributions. The results have been compared with both the experimental data and the numerical results in the literatures. Good agreement is obtained in the studied cases and the developed model overcomes the false secondary Nusselt number peak in high nozzle-plate spacing for slot jets which is predicted by the standard SST k-omega model. The results show that the modifications improve the model's ability to predict the heat transfer for jet impingement by reinforcing the model's sensitivity to the pressure gradient. By way of comparative studies, it shows that the SST k-omega with transition model and the standard SST k-omega model are not sensitive to the pressure gradient. Meanwhile, the cases of nozzle-plate spacing of 2 and 6 are also investigated. This investigation indicates that the pressure gradient plays an important role for turbulent slot impinging jet. And it also reveals that the effect of cross-diffusion term should not be ignored in the boundary layer. (C) 2019 Elsevier Ltd. All rights reserved.
机译:本文已经开发了一种基于OpenFoam的湍流模型,用于喷射冲击传热基于标准SST k-Omega模型,并考虑交叉扩散项和Kato-Limunde模型的影响。在压力分布,平均速度,皮肤摩擦和局部营养数分布方面,研究了修改的效果4和9.2的不同喷嘴板间隔。结果与实验数据和文献中的数值结果进行了比较。在研究的情况下获得了良好的一致性,并且开发的模型克服了标准SSTK-Omega模型预测的槽喷射中的高喷嘴板间距中的假次级露珠数峰值。结果表明,通过加强模型对压力梯度的敏感性,修改改善了模型预测喷射冲击的热传递的能力。通过比较研究,它表明,具有转换模型的SST k-Omega和标准SST k-Omega模型对压力梯度不敏感。同时,还研究了2和6的喷嘴板间距的情况。本研究表明,压力梯度对湍流槽撞击喷射起着重要作用。它还揭示了在边界层中不应忽视交叉扩散项的效果。 (c)2019 Elsevier Ltd.保留所有权利。

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  • 作者单位

    Dalian Univ Technol Sch Naval Architecture Liaoning Engn Lab Deep Sea Floating Struct Dalian 116024 Peoples R China;

    Dalian Univ Technol Sch Naval Architecture Liaoning Engn Lab Deep Sea Floating Struct Dalian 116024 Peoples R China;

    Dalian Univ Technol Sch Naval Architecture Liaoning Engn Lab Deep Sea Floating Struct Dalian 116024 Peoples R China|Dalian Univ Technol State Key Lab Struct Anal Ind Equipment Dalian 116024 Peoples R China|Collaborat Innovat Ctr Adv Ship & Deep Sea Explor Shanghai 200240 Peoples R China;

    China Natl Offshore Oil Corp Res Inst Ltd Beijing 100027 Peoples R China;

    Beijing Inst Astronaut Syst Engn Beijing 100076 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Jet impingement; Heat transfer; Cross-diffusion term; Pressure gradient; OpenFOAM;

    机译:喷射冲击;传热;交叉扩散项;压力梯度;OpenFoam;

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