Effect of secondary fluid injection on flow through supersonic nozzle

IF 1.7 4区 计算机科学 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Dakshina Murthy Inturi, Lovaraju Pinnam, Ramachandra Raju Vegesna, Ethirajan Rathakrishnan
{"title":"Effect of secondary fluid injection on flow through supersonic nozzle","authors":"Dakshina Murthy Inturi, Lovaraju Pinnam, Ramachandra Raju Vegesna, Ethirajan Rathakrishnan","doi":"10.1007/s12650-024-01013-w","DOIUrl":null,"url":null,"abstract":"<h3 data-test=\"abstract-sub-heading\">Abstract</h3><p>The effect of secondary gas injection on the flow through an axisymmetric Mach 2 nozzle is studied experimentally. The experiments were conducted for a nozzle pressure ratio of 5. The secondary injection locations chosen for this study were <i>L</i><sub>s</sub> = 0.5<i>L</i><sub>d</sub> and 0.75<i>L</i><sub>d</sub>, and the secondary gas was injected at secondary pressure ratios (SPR) 0.5, 1.0, and 1.5. It is found that for injection at 0.5 <i>L</i><sub>d</sub>, the flow emanating is not deflected for all SPRs. For injection at 0.75 <i>L</i><sub>d</sub>, the flow is deflected by about 5.5<sup>0</sup>, 5.5<sup>0</sup> and 10<sup>0</sup>, for SPRs 0.5, 1.0, and 1.5, respectively. These flow deflections are observed only in the plane of injection. The effect of secondary injection was not observed in the plane normal to the secondary injection.</p><h3 data-test=\"abstract-sub-heading\">Graphical abstract</h3>\n","PeriodicalId":54756,"journal":{"name":"Journal of Visualization","volume":"19 1","pages":""},"PeriodicalIF":1.7000,"publicationDate":"2024-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Visualization","FirstCategoryId":"94","ListUrlMain":"https://doi.org/10.1007/s12650-024-01013-w","RegionNum":4,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS","Score":null,"Total":0}
引用次数: 0

Abstract

The effect of secondary gas injection on the flow through an axisymmetric Mach 2 nozzle is studied experimentally. The experiments were conducted for a nozzle pressure ratio of 5. The secondary injection locations chosen for this study were Ls = 0.5Ld and 0.75Ld, and the secondary gas was injected at secondary pressure ratios (SPR) 0.5, 1.0, and 1.5. It is found that for injection at 0.5 Ld, the flow emanating is not deflected for all SPRs. For injection at 0.75 Ld, the flow is deflected by about 5.50, 5.50 and 100, for SPRs 0.5, 1.0, and 1.5, respectively. These flow deflections are observed only in the plane of injection. The effect of secondary injection was not observed in the plane normal to the secondary injection.

Graphical abstract

Abstract Image

二次流体注入对超音速喷嘴流动的影响
摘要 通过实验研究了二次气体注入对通过轴对称马赫数为 2 的喷嘴的流动的影响。实验是在喷嘴压力比为 5 时进行的。本研究选择的二次喷射位置为 Ls = 0.5Ld 和 0.75Ld,二次气体喷射的二次压力比 (SPR) 为 0.5、1.0 和 1.5。结果发现,以 0.5 Ld 注入时,在所有 SPR 下喷出的气流都不会偏转。当注入 0.75 Ld 时,SPR 值为 0.5、1.0 和 1.5 时,气流分别偏转了约 5.50、5.50 和 100。这些流动偏转仅在注入平面内观察到。在二次注入的法线平面上没有观察到二次注入的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Journal of Visualization
Journal of Visualization COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS-IMAGING SCIENCE & PHOTOGRAPHIC TECHNOLOGY
CiteScore
3.40
自引率
5.90%
发文量
79
审稿时长
>12 weeks
期刊介绍: Visualization is an interdisciplinary imaging science devoted to making the invisible visible through the techniques of experimental visualization and computer-aided visualization. The scope of the Journal is to provide a place to exchange information on the latest visualization technology and its application by the presentation of latest papers of both researchers and technicians.
×
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