Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions
Author:
Affiliation:
1. School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang 150001, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053547
Reference24 articles.
1. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow
2. Experimental Investigation of the Unstart Process of a Generic Hypersonic Inlet
3. Experimental Investigation of the Shock Train in an Isolator of a Scramjet Inlet
4. Novel Oscillatory Patterns of Hypersonic Inlet Buzz
5. CIAM/NASA Mach 6.5 scramjet flight and ground test
Cited by 38 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. Low-frequency unsteadiness mechanisms of unstart flow in an inlet with rectangular-to-elliptical shape transition under off-design condition at a Mach number of 4;Journal of Fluid Mechanics;2024-07-25
2. Mode transition control law analysis of ammonia MIPCC aeroengine considering inlet–compressor safety matching;Energy;2024-02
3. Hysteresis behavior of shock train driven by continuous incoming Mach number variation in an isolator with background waves;European Journal of Mechanics - B/Fluids;2023-09
4. Scramjet combustion with bumpy struts;Aerospace Science and Technology;2023-09
5. Numerical investigation of the unstart flow at off-design condition of REST inlet at a Mach of 4;Aerospace Science and Technology;2023-05
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