Thermal behavior of an isolator with mode transition inducing back-pressure of a dual-mode scramjet
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference23 articles.
1. Experimental study on effects of fuel injection on scramjet combustor performance;Wu;Chin J Aeronaut,2007
2. Experimental investigation of hydrocarbon-fuel ignition in scramjet combustor;Song;Chin J Aeronaut,2004
3. Survey on the mode transition technique in combined cycle propulsion systems;Huang;Aerosp Sci Technol,2014
4. Experimental study of a dual-mode scramjet isolator;Le;J Propul Power,2008
5. Unstart detection in a simplified-geometry hypersonic inlet-isolator flow;Srikant;J Propul Power,2010
Cited by 15 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. Parametric Study of Flow and Combustion Characteristic in a Cavitied Scramjet with Multi-Position Injection;Fire;2024-05-22
2. The influence of supersonic spatial-temporal coupling disturbance on detonation in an expanded chamber;Aerospace Science and Technology;2024-04
3. Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range;Chinese Journal of Aeronautics;2023-12
4. Mixing and combustion characteristics in a scramjet combustor with different distances between cavity and backward-facing step;Chinese Journal of Aeronautics;2023-07
5. Flow and heat transfer of hydrocarbon fuel in the double-layer regenerative cooling channels;Numerical Heat Transfer, Part A: Applications;2023-04-25
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