Calculation of the Flow Structure in the Interaction with the Counterflow of a Jet Flowing from the Frontal Surface of a Body of Revolution

IF 1 4区 工程技术 Q4 MECHANICS Fluid Dynamics Pub Date : 2024-03-24 DOI:10.1134/S0015462823602681
A. V. Panasenko
{"title":"Calculation of the Flow Structure in the Interaction with the Counterflow of a Jet Flowing from the Frontal Surface of a Body of Revolution","authors":"A. V. Panasenko","doi":"10.1134/S0015462823602681","DOIUrl":null,"url":null,"abstract":"<p>The results of the calculation of the interaction of a supersonic jet flowing at a zero angle of attack from the frontal surface of the body of rotation to the opposite supersonic flow at different supersonic Mach numbers of the flow and jet are given. The influence of the total pressure in the gas flow and in the jet on the structure of the emerging gas flow is considered.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"58 8","pages":"1568 - 1576"},"PeriodicalIF":1.0000,"publicationDate":"2024-03-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Fluid Dynamics","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1134/S0015462823602681","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0

Abstract

The results of the calculation of the interaction of a supersonic jet flowing at a zero angle of attack from the frontal surface of the body of rotation to the opposite supersonic flow at different supersonic Mach numbers of the flow and jet are given. The influence of the total pressure in the gas flow and in the jet on the structure of the emerging gas flow is considered.

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
计算从旋转体正面流出的喷流与逆流相互作用时的流动结构
摘要 本文给出了在不同超音速马赫数的气流和射流条件下,以零攻角从旋转体正面流向对面超音速气流的超音速射流相互作用的计算结果。考虑了气流和射流中的总压力对新出现的气流结构的影响。
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 去求助
来源期刊
Fluid Dynamics
Fluid Dynamics MECHANICS-PHYSICS, FLUIDS & PLASMAS
CiteScore
1.30
自引率
22.20%
发文量
61
审稿时长
6-12 weeks
期刊介绍: Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.
期刊最新文献
Development of the Deposit Formation Similarity Criterion with the Electrochemical Number Direct Statistical Modeling of Oxygen Radiation behind a Shock Wave Treatment of the Thermal Nonequilibrium and Ionization Effects on the Refractive Index of a Reacting Gas: Atmospheric Air and Combustion Products Formation of Three-Phase Cavitation Bubbles with Their Own Electric Field in a Hydrophobic Liquid Numerical Simulation of Vapor Bulk Condensation near the Interfacial Surface under Intensive Evaporation Conditions
×
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