高度变化条件下双钟形喷嘴横向喷射的参数化研究

IF 1.7 4区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Propulsion and Power Pub Date : 2023-08-02 DOI:10.2514/1.b39077
Brian Legros, L. Léger, A. Kourta, A. Chpoun, M. Sellam
{"title":"高度变化条件下双钟形喷嘴横向喷射的参数化研究","authors":"Brian Legros, L. Léger, A. Kourta, A. Chpoun, M. Sellam","doi":"10.2514/1.b39077","DOIUrl":null,"url":null,"abstract":"The dual-bell nozzle (DBN) is a rocket nozzle concept that could provide a substantial payload gain. The present paper focuses on the impact of radial secondary injection on DBN behavior during its ascent and descent in the atmosphere. The influence of the secondary injection settling chamber (cavity) volume is discussed. The positive influence of the cavity volume on the DBN behavior during transition phases has been exposed, and its effects during retransition were shown to be negligible. The use of secondary injection allowed the transition nozzle pressure ratio to be increased by nearly 24%, and the lateral forces were reduced to less than 1% of the nozzle thrust. A first approach regarding secondary injection optimization is finally proposed.","PeriodicalId":16903,"journal":{"name":"Journal of Propulsion and Power","volume":" ","pages":""},"PeriodicalIF":1.7000,"publicationDate":"2023-08-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions\",\"authors\":\"Brian Legros, L. Léger, A. Kourta, A. Chpoun, M. Sellam\",\"doi\":\"10.2514/1.b39077\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The dual-bell nozzle (DBN) is a rocket nozzle concept that could provide a substantial payload gain. The present paper focuses on the impact of radial secondary injection on DBN behavior during its ascent and descent in the atmosphere. The influence of the secondary injection settling chamber (cavity) volume is discussed. The positive influence of the cavity volume on the DBN behavior during transition phases has been exposed, and its effects during retransition were shown to be negligible. The use of secondary injection allowed the transition nozzle pressure ratio to be increased by nearly 24%, and the lateral forces were reduced to less than 1% of the nozzle thrust. A first approach regarding secondary injection optimization is finally proposed.\",\"PeriodicalId\":16903,\"journal\":{\"name\":\"Journal of Propulsion and Power\",\"volume\":\" \",\"pages\":\"\"},\"PeriodicalIF\":1.7000,\"publicationDate\":\"2023-08-02\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Propulsion and Power\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.2514/1.b39077\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Propulsion and Power","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2514/1.b39077","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

摘要

双钟形喷嘴(DBN)是一种火箭喷嘴概念,可以提供可观的有效载荷增益。本文主要研究径向二次喷射对DBN在大气中上升和下降过程的影响。讨论了二次注射沉降室(腔)体积的影响。在转变阶段,空腔体积对DBN行为的积极影响已经暴露出来,而在再转变期间,它的影响被证明是可以忽略不计的。二次喷射的使用使过渡喷嘴的压力比提高了近24%,横向力降低到喷嘴推力的1%以下。最后提出了二次注入优化的第一种方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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
Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions
The dual-bell nozzle (DBN) is a rocket nozzle concept that could provide a substantial payload gain. The present paper focuses on the impact of radial secondary injection on DBN behavior during its ascent and descent in the atmosphere. The influence of the secondary injection settling chamber (cavity) volume is discussed. The positive influence of the cavity volume on the DBN behavior during transition phases has been exposed, and its effects during retransition were shown to be negligible. The use of secondary injection allowed the transition nozzle pressure ratio to be increased by nearly 24%, and the lateral forces were reduced to less than 1% of the nozzle thrust. A first approach regarding secondary injection optimization is finally proposed.
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
Journal of Propulsion and Power
Journal of Propulsion and Power 工程技术-工程:宇航
CiteScore
4.20
自引率
21.10%
发文量
97
审稿时长
6.5 months
期刊介绍: This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. Papers in these disciplines and the sciences of combustion, fluid mechanics, and solid mechanics as directly related to propulsion and power are solicited.
期刊最新文献
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles Fuel Temperature Effects on Combustion Stability of a High-Pressure Liquid-Fueled Swirl Flame Optimization of Thrust of a Generic X-51 Hypersonic Vehicle Application of Boundary Layer Combustion in High-Mach-Number Scramjets
×
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