Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference38 articles.
1. Mixing characteristics of vent slot mixer in supersonic flow;Kim;Aerosp. Sci. Technol.,2016
2. Quasi-1D analysis and performance estimation of a sub-scale RBCC engine with chemical equilibrium;Kim;Aerosp. Sci. Technol.,2017
3. Rapid supersonic performance estimation for a novel RBCC engine inlet;Murzionak;Aerosp. Sci. Technol.,2014
4. Survey on the mode transition technique in combined cycle propulsion systems;Huang;Aerosp. Sci. Technol.,2014
5. Numerical investigation of shock train unsteady movement in a mixing duct;Lu;Aerosp. Sci. Technol.,2018
Cited by 35 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Experimental investigation on performance variation and dynamic characteristics of a variable geometry rocket-based combined cycle combustor;Aerospace Science and Technology;2024-10
2. Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber;Defence Technology;2024-09
3. Dynamic flow behaviors of an inlet isolator in embedded rocket-driven mode transitions;Physics of Fluids;2024-07-01
4. Combustion organization strategies for a variable geometry RBCC combustor under low total temperature conditions;Applied Thermal Engineering;2024-01
5. Experimental and numerical study on low-temperature supersonic ejector;International Journal of Thermofluids;2023-11
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