Combustion Induced Choking and Unstart Initiation in a Circular Constant-Area Supersonic Flow
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057921
Reference48 articles.
1. AIAA Education Series;Heiser W. H.,1993
2. Recent research progress on unstart mechanism, detection and control of hypersonic inlet
3. Unstart phenomena induced by flow choking in scramjet inlet-isolators
4. B. One-Dimensional Treatment of Steady Gas Dynamics
5. The Mechanism of Pseudo-Shock Waves
Cited by 23 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. Numerical investigation on flow choking induced by local heat release and large-scale flow separation in a supersonic combustor;Combustion and Flame;2024-10
2. Nitric Oxide and Temperature Measurement Using Laser Absorption Spectroscopy in Arc-Heater Plenum;AIAA Journal;2024-09-03
3. Investigation of multi-scale flow structures and combustion characteristics in a cavity-enhanced circular scramjet;Combustion and Flame;2024-06
4. Fluid and Combustion Dynamics in Axisymmetric and Perisymmetric Supersonic Combustion Flowpaths;AIAA Journal;2024-06
5. Investigation of Fuel Mixing in Cavity Flameholder with Energy-Tuned Laser-Induced Breakdown Spectroscopy;AIAA SCITECH 2024 Forum;2024-01-04
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