Liquid Jet Breakup and Penetration in a Gas Cross-Flow -An Experimental Study

IF 1.5 4区 工程技术 Q3 ENGINEERING, MECHANICAL Experimental Techniques Pub Date : 2023-08-22 DOI:10.1007/s40799-023-00668-8
M. Pourrousta, M. M. Larimi, M. Biglarian, P. Hedayati
{"title":"Liquid Jet Breakup and Penetration in a Gas Cross-Flow -An Experimental Study","authors":"M. Pourrousta,&nbsp;M. M. Larimi,&nbsp;M. Biglarian,&nbsp;P. Hedayati","doi":"10.1007/s40799-023-00668-8","DOIUrl":null,"url":null,"abstract":"<div><p>In the present study, an experimental platform is developed to study the behavior of the injected jet in a gas cross-flow applicable to different categories of fluid mechanics such as combustion. In all tests, water and air are used as jet and cross-flow gas, respectively. The main target of this work is to cover the higher range of momentum ratios and Weber numbers for the presentation of a more accurate equation for jet trajectory. To achieve a desirable scale of experiments, the range of momentum ratio is considered from 5 to 211 and the Weber number of gasses in all tests is between 1.1–19.1. For data mining and measurements, the shadowgraph method is used. It is shown that by increasing the momentum ratio (about 84%), the breakup point height is increased (about 94%). Three different types of breakups were observed in the tests. It observed that as the Weber number increases, the type of jet column mechanism changes. It also revealed that the type of breakup mechanism would not have a significant effect on the jet trajectory. In addition, it demonstrated that the momentum ratio parameter would have a decisive role in the direction of jet motion, and as the momentum ratio increases, the jet column height increases. Finally, an equation for the trajectory of jet flight under all test conditions is presented.</p></div>","PeriodicalId":553,"journal":{"name":"Experimental Techniques","volume":"48 3","pages":"449 - 459"},"PeriodicalIF":1.5000,"publicationDate":"2023-08-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Experimental Techniques","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s40799-023-00668-8","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0

Abstract

In the present study, an experimental platform is developed to study the behavior of the injected jet in a gas cross-flow applicable to different categories of fluid mechanics such as combustion. In all tests, water and air are used as jet and cross-flow gas, respectively. The main target of this work is to cover the higher range of momentum ratios and Weber numbers for the presentation of a more accurate equation for jet trajectory. To achieve a desirable scale of experiments, the range of momentum ratio is considered from 5 to 211 and the Weber number of gasses in all tests is between 1.1–19.1. For data mining and measurements, the shadowgraph method is used. It is shown that by increasing the momentum ratio (about 84%), the breakup point height is increased (about 94%). Three different types of breakups were observed in the tests. It observed that as the Weber number increases, the type of jet column mechanism changes. It also revealed that the type of breakup mechanism would not have a significant effect on the jet trajectory. In addition, it demonstrated that the momentum ratio parameter would have a decisive role in the direction of jet motion, and as the momentum ratio increases, the jet column height increases. Finally, an equation for the trajectory of jet flight under all test conditions is presented.

Abstract Image

Abstract Image

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
气体横流中的液体射流破裂和穿透 - 实验研究
本研究开发了一个实验平台,用于研究气体横流中喷射射流的行为,适用于燃烧等不同类别的流体力学。在所有测试中,水和空气分别用作射流和横流气体。这项工作的主要目标是覆盖更高的动量比和韦伯数范围,以提出更精确的射流轨迹方程。为了达到理想的实验规模,动量比的范围从 5 到 211,所有测试中气体的韦伯数都在 1.1-19.1 之间。数据挖掘和测量采用了阴影图法。结果表明,通过增加动量比(约 84%),破裂点高度增加了(约 94%)。测试中观察到三种不同类型的破裂。试验观察到,随着韦伯数字的增加,喷射柱机制的类型也发生了变化。研究还发现,断裂机制类型对射流轨迹的影响不大。此外,研究还证明动量比参数对射流运动方向具有决定性作用,而且随着动量比的增加,射流柱高度也会增加。最后,提出了在所有试验条件下的喷流飞行轨迹方程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Experimental Techniques
Experimental Techniques 工程技术-材料科学:表征与测试
CiteScore
3.50
自引率
6.20%
发文量
88
审稿时长
5.2 months
期刊介绍: Experimental Techniques is a bimonthly interdisciplinary publication of the Society for Experimental Mechanics focusing on the development, application and tutorial of experimental mechanics techniques. The purpose for Experimental Techniques is to promote pedagogical, technical and practical advancements in experimental mechanics while supporting the Society''s mission and commitment to interdisciplinary application, research and development, education, and active promotion of experimental methods to: - Increase the knowledge of physical phenomena - Further the understanding of the behavior of materials, structures, and systems - Provide the necessary physical observations necessary to improve and assess new analytical and computational approaches.
期刊最新文献
On the Cover: Identification of Lightning Strike Damage Severity Using Pulse Thermography Through Integration of Thermal Data A Note of Gratitude from the Editor-in-Chief On the Cover: Study on Velocity Distribution on Cross-Section Flow of T-Shunt Reconstruction of Unsteady Lift Force Measurements Using Non-Dimensional Scaling Optimization Surface Microstructure Evolution and Mechanical Property Investigation of Inconel 718 Alloy Using Multiple Trimmings and WEDM
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1