Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-09-11 DOI:10.1108/aeat-05-2024-0137
Prabhu Paramasivam, Sami Al Obaid, Arun Balasubramanian
{"title":"Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design","authors":"Prabhu Paramasivam, Sami Al Obaid, Arun Balasubramanian","doi":"10.1108/aeat-05-2024-0137","DOIUrl":null,"url":null,"abstract":"<h3>Purpose</h3>\n<p>This study aims to numerically analyse a full-scale burner across a wide range of operating pressure conditions and determine the effect of swirl velocity on flame stabilization, flame holding and combustion performance.</p><!--/ Abstract__block -->\n<h3>Design/methodology/approach</h3>\n<p>This study uses a numerical analysis approach to investigate a three-dimensional full-scale burner. Modified governing equations are used to determine the effect of swirl velocity on flame stabilization and flame holding. The GR-Mech 3.0 chemical reaction mechanism is used to predict the combustion process. To validate the model, a grid independence study is performed.</p><!--/ Abstract__block -->\n<h3>Findings</h3>\n<p>The study reveals that swirl velocity enhances flame stability, resulting in better combustion rates. As the swirl velocity increases, higher flame temperatures are observed due to high convective heat recirculation. The heat transfer coefficient and high radiative extinction coefficient are found to vary based on fuel swirl velocity. The mass fraction of CH<sub>4</sub> and CO emphasizes the role of swirl velocity on flame structure. Increasing velocity potentially improves combustion by delaying the process, leading to better combustion and lower emissions.</p><!--/ Abstract__block -->\n<h3>Originality/value</h3>\n<p>The findings of this study contribute to the understanding of swirl-stabilized combustion and can guide the development of advanced combustion technologies, making it a valuable addition to the existing combustion field.</p><!--/ Abstract__block -->","PeriodicalId":55540,"journal":{"name":"Aircraft Engineering and Aerospace Technology","volume":"17 1","pages":""},"PeriodicalIF":1.2000,"publicationDate":"2024-09-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aircraft Engineering and Aerospace Technology","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1108/aeat-05-2024-0137","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Purpose

This study aims to numerically analyse a full-scale burner across a wide range of operating pressure conditions and determine the effect of swirl velocity on flame stabilization, flame holding and combustion performance.

Design/methodology/approach

This study uses a numerical analysis approach to investigate a three-dimensional full-scale burner. Modified governing equations are used to determine the effect of swirl velocity on flame stabilization and flame holding. The GR-Mech 3.0 chemical reaction mechanism is used to predict the combustion process. To validate the model, a grid independence study is performed.

Findings

The study reveals that swirl velocity enhances flame stability, resulting in better combustion rates. As the swirl velocity increases, higher flame temperatures are observed due to high convective heat recirculation. The heat transfer coefficient and high radiative extinction coefficient are found to vary based on fuel swirl velocity. The mass fraction of CH4 and CO emphasizes the role of swirl velocity on flame structure. Increasing velocity potentially improves combustion by delaying the process, leading to better combustion and lower emissions.

Originality/value

The findings of this study contribute to the understanding of swirl-stabilized combustion and can guide the development of advanced combustion technologies, making it a valuable addition to the existing combustion field.

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
火焰稳定和减排:氢燃料燃烧器设计中漩涡速度影响的综合研究
设计/方法/途径 本研究采用数值分析方法研究三维全尺寸燃烧器。修改后的控制方程用于确定漩涡速度对火焰稳定和火焰保持的影响。使用 GR-Mech 3.0 化学反应机制预测燃烧过程。研究结果研究结果表明,漩涡速度可增强火焰稳定性,从而提高燃烧率。随着漩涡速度的增加,由于高对流热再循环,可观察到更高的火焰温度。研究发现,传热系数和高辐射消光系数随燃料漩涡速度的变化而变化。CH4 和 CO 的质量分数强调了漩涡速度对火焰结构的作用。提高漩涡速度可通过延迟燃烧过程来改善燃烧,从而提高燃烧效果并降低排放。
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
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
期刊最新文献
Wind tunnel investigation of hemispherical forebody interaction on the drag coefficient of a D-shaped model Parameter tuning for active disturbance rejection control of fixed-wing UAV based on improved bald eagle search algorithm Integrating urban air mobility into smart cities: a proposal for relevant use cases in the next decades Heavy fuel preparation effects on the operation of a spark ignition unmanned aerial vehicle engine Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design
×
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