Effects of injector spacing and momentum flux ratio on combustion instability in a model chamber with gas-centered swirl coaxial injectors
Author:
Funder
National Research Foundation of Korea
Ministry of Trade, Industry and Energy
Ministry of Science, ICT and Future Planning
Korea Institute of Energy Technology Evaluation and Planning
Publisher
Elsevier BV
Reference50 articles.
1. Effects of fuel line acoustics on the self-excited combustion instability mode transition with hydrogen-enriched laboratory-scale partially premixed combustor;Kim;Int. J. Hydrog. Energy,2020
2. Numerical simulation of the combustion stability of natural gas and syngas in a surface-stabilized combustion burner;Arrieta;J. Phys. Conf. Ser.,2019
3. Spray patterns and injection characteristics of gas-centered swirl coaxial injectors;Son;J. Aerospace Eng.,2017
4. Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector;Dai;Aerosp. Sci. Technol.,2018
5. Experimental study on the flow field distribution characteristics of a gas–liquid swirl coaxial injector under ambient pressure;Chen;Aerosp. Sci. Technol.,2021
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3