Numerical simulation of powder fuel mixing characteristics in supersonic circular combustion chamber

IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL
Wenxue Han , Chunbo Hu , Junjie Li , Jiaxin Dong , Rong Lei , Chao Li
{"title":"Numerical simulation of powder fuel mixing characteristics in supersonic circular combustion chamber","authors":"Wenxue Han ,&nbsp;Chunbo Hu ,&nbsp;Junjie Li ,&nbsp;Jiaxin Dong ,&nbsp;Rong Lei ,&nbsp;Chao Li","doi":"10.1016/j.ijheatfluidflow.2025.110002","DOIUrl":null,"url":null,"abstract":"<div><div>To explore the combustion organization of a powder-fueled scramjets, a numerical investigation was conducted to analyze powder fuel mixing characteristics in supersonic combustors. This study systematically investigates particle-air mixing dynamics in a supersonic circular cavity-based combustor through parametric variations of injection positions and swirl angles. Subsequently, an innovative partially-covered cavity configuration is proposed, and its mixing efficiency is evaluated under different injection angles. Numerical simulations demonstrated that in leading-edge injection configurations, the transverse jet-induced bow shock caused deflection of the X-shaped shockwave system toward the injection port in the annular combustor. Comparatively, direct particle injection into the cavity recirculation zone enhanced particle residence time; For upper-wall injection configurations, particle residence time (τ) in exhibited a positive correlation with swirl injection angle(θ), reaching τ = 9 ms at θ = 90°; In partially-covered cavity configurations, swirl injection of fuel enhanced particle residence, with optimal performance achieved at Lc = 35 mm and θ = 60°, and the particle mixing degree reached about 0.8.</div></div>","PeriodicalId":335,"journal":{"name":"International Journal of Heat and Fluid Flow","volume":"117 ","pages":"Article 110002"},"PeriodicalIF":2.6000,"publicationDate":"2025-08-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Heat and Fluid Flow","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0142727X25002607","RegionNum":3,"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

Abstract

To explore the combustion organization of a powder-fueled scramjets, a numerical investigation was conducted to analyze powder fuel mixing characteristics in supersonic combustors. This study systematically investigates particle-air mixing dynamics in a supersonic circular cavity-based combustor through parametric variations of injection positions and swirl angles. Subsequently, an innovative partially-covered cavity configuration is proposed, and its mixing efficiency is evaluated under different injection angles. Numerical simulations demonstrated that in leading-edge injection configurations, the transverse jet-induced bow shock caused deflection of the X-shaped shockwave system toward the injection port in the annular combustor. Comparatively, direct particle injection into the cavity recirculation zone enhanced particle residence time; For upper-wall injection configurations, particle residence time (τ) in exhibited a positive correlation with swirl injection angle(θ), reaching τ = 9 ms at θ = 90°; In partially-covered cavity configurations, swirl injection of fuel enhanced particle residence, with optimal performance achieved at Lc = 35 mm and θ = 60°, and the particle mixing degree reached about 0.8.
超声速圆形燃烧室粉末燃料混合特性的数值模拟
为了探索粉末燃料超燃冲压发动机的燃烧组织,对超声速燃烧室内粉末燃料混合特性进行了数值研究。本文通过改变喷射位置和旋流角的参数,系统地研究了超音速圆腔燃烧室中颗粒-空气的混合动力学。随后,提出了一种创新的部分覆盖腔结构,并对其在不同喷射角度下的混合效率进行了评估。数值模拟表明,在前缘喷射构型下,横向射流诱导的弓形激波使环形燃烧室内的x形激波系统向喷射口偏转。相比之下,将颗粒直接注入腔体再循环区可以延长颗粒的停留时间;对于上壁喷射构型,粒子停留时间(τ)与旋流喷射角(θ)呈正相关,在θ = 90°处达到τ = 9 ms;在部分覆盖型腔构型下,燃油旋流喷射增强了颗粒停留,在Lc = 35 mm、θ = 60°时性能最佳,颗粒混合度约为0.8。
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
International Journal of Heat and Fluid Flow
International Journal of Heat and Fluid Flow 工程技术-工程:机械
CiteScore
5.00
自引率
7.70%
发文量
131
审稿时长
33 days
期刊介绍: The International Journal of Heat and Fluid Flow welcomes high-quality original contributions on experimental, computational, and physical aspects of convective heat transfer and fluid dynamics relevant to engineering or the environment, including multiphase and microscale flows. Papers reporting the application of these disciplines to design and development, with emphasis on new technological fields, are also welcomed. Some of these new fields include microscale electronic and mechanical systems; medical and biological systems; and thermal and flow control in both the internal and external environment.
×
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:604180095
Book学术官方微信