测量撞击多可压缩射流的局部努塞尔特数和局部恢复因子

IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL
H.I. Shaikh , S. Siddapureddy , S.V. Prabhu
{"title":"测量撞击多可压缩射流的局部努塞尔特数和局部恢复因子","authors":"H.I. Shaikh ,&nbsp;S. Siddapureddy ,&nbsp;S.V. Prabhu","doi":"10.1016/j.expthermflusci.2024.111320","DOIUrl":null,"url":null,"abstract":"<div><div>In the present study the appropriate reference temperature is identified for the compressible impinging jet. Using the measured reference temperature, local recovery factor is calculated. The steady state thin metal foil technique is used for the measurement of target plate temperature. In this study, the effect of Mach number (<em>Ma</em>) at a constant Reynolds number (<em>Re</em>) and the combined effect of Mach number and Reynolds number on the heat transfer rate are investigated. For both the cases, jet-to-plate distance is varied from <em>z/d</em> = 5 to 12. For the first case (effect of Mach number at a constant <em>Re</em> = 20,000), <em>Ma</em> is varied from 0.15 to 0.85. In the second case (combined effect of Mach number and Reynolds number), <em>Ma</em> is varied from 0.2 to 0.78 and the corresponding <em>Re</em> variation is 7200 to 29,000. At a constant Reynolds number, the heat transfer coefficient increases with the increase in the Mach number. For a given Mach number and Reynolds number, the heat transfer rate decreases with the increase in the jet-to-plate distance. The recovery factor remains unaffected by the Mach number and jet-to-plate distance in the case of the concurrent variation of the Mach number and Reynolds number.</div></div>","PeriodicalId":12294,"journal":{"name":"Experimental Thermal and Fluid Science","volume":"160 ","pages":"Article 111320"},"PeriodicalIF":2.8000,"publicationDate":"2024-09-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Measurement of local Nusselt number and local recovery factor for impinging multiple compressible jets\",\"authors\":\"H.I. Shaikh ,&nbsp;S. Siddapureddy ,&nbsp;S.V. Prabhu\",\"doi\":\"10.1016/j.expthermflusci.2024.111320\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>In the present study the appropriate reference temperature is identified for the compressible impinging jet. Using the measured reference temperature, local recovery factor is calculated. The steady state thin metal foil technique is used for the measurement of target plate temperature. In this study, the effect of Mach number (<em>Ma</em>) at a constant Reynolds number (<em>Re</em>) and the combined effect of Mach number and Reynolds number on the heat transfer rate are investigated. For both the cases, jet-to-plate distance is varied from <em>z/d</em> = 5 to 12. For the first case (effect of Mach number at a constant <em>Re</em> = 20,000), <em>Ma</em> is varied from 0.15 to 0.85. In the second case (combined effect of Mach number and Reynolds number), <em>Ma</em> is varied from 0.2 to 0.78 and the corresponding <em>Re</em> variation is 7200 to 29,000. At a constant Reynolds number, the heat transfer coefficient increases with the increase in the Mach number. For a given Mach number and Reynolds number, the heat transfer rate decreases with the increase in the jet-to-plate distance. The recovery factor remains unaffected by the Mach number and jet-to-plate distance in the case of the concurrent variation of the Mach number and Reynolds number.</div></div>\",\"PeriodicalId\":12294,\"journal\":{\"name\":\"Experimental Thermal and Fluid Science\",\"volume\":\"160 \",\"pages\":\"Article 111320\"},\"PeriodicalIF\":2.8000,\"publicationDate\":\"2024-09-18\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Experimental Thermal and Fluid Science\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0894177724001894\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Experimental Thermal and Fluid Science","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0894177724001894","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0

摘要

本研究为可压缩撞击射流确定了适当的参考温度。利用测得的参考温度计算局部恢复系数。稳态薄金属箔技术用于测量目标板温度。在这项研究中,研究了马赫数(Ma)在雷诺数(Re)恒定时的影响,以及马赫数和雷诺数对传热速率的综合影响。在这两种情况下,射流到板的距离在 z/d = 5 到 12 之间变化。在第一种情况下(马赫数在恒定 Re = 20,000 条件下的影响),Ma 的变化范围为 0.15 至 0.85。在第二种情况下(马赫数和雷诺数的综合影响),Ma 的变化范围为 0.2 至 0.78,相应的 Re 变化范围为 7200 至 29000。在雷诺数不变的情况下,传热系数随着马赫数的增加而增加。在给定的马赫数和雷诺数下,热传导率随着射流到平板距离的增加而降低。在马赫数和雷诺数同时变化的情况下,恢复系数不受马赫数和喷射板间距的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Measurement of local Nusselt number and local recovery factor for impinging multiple compressible jets
In the present study the appropriate reference temperature is identified for the compressible impinging jet. Using the measured reference temperature, local recovery factor is calculated. The steady state thin metal foil technique is used for the measurement of target plate temperature. In this study, the effect of Mach number (Ma) at a constant Reynolds number (Re) and the combined effect of Mach number and Reynolds number on the heat transfer rate are investigated. For both the cases, jet-to-plate distance is varied from z/d = 5 to 12. For the first case (effect of Mach number at a constant Re = 20,000), Ma is varied from 0.15 to 0.85. In the second case (combined effect of Mach number and Reynolds number), Ma is varied from 0.2 to 0.78 and the corresponding Re variation is 7200 to 29,000. At a constant Reynolds number, the heat transfer coefficient increases with the increase in the Mach number. For a given Mach number and Reynolds number, the heat transfer rate decreases with the increase in the jet-to-plate distance. The recovery factor remains unaffected by the Mach number and jet-to-plate distance in the case of the concurrent variation of the Mach number and Reynolds number.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Experimental Thermal and Fluid Science
Experimental Thermal and Fluid Science 工程技术-工程:机械
CiteScore
6.70
自引率
3.10%
发文量
159
审稿时长
34 days
期刊介绍: Experimental Thermal and Fluid Science provides a forum for research emphasizing experimental work that enhances fundamental understanding of heat transfer, thermodynamics, and fluid mechanics. In addition to the principal areas of research, the journal covers research results in related fields, including combined heat and mass transfer, flows with phase transition, micro- and nano-scale systems, multiphase flow, combustion, radiative transfer, porous media, cryogenics, turbulence, and novel experimental techniques.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信