Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference43 articles.
1. Thermal behavior of an isolator with mode transition inducing back-pressure of a dual-mode scramjet;Yang;Chin J Aeronaut,2017
2. A brief review on the recent advances in scramjet engine;Choubey;AIP Conf Proc,2017
3. Mohieldin T, Tiwari S, Olynciw M. Asymmetric flow-structures in dual mode scramjet combustor with significant upstream interaction. Reston: AIAA; 2001. Report No.: AIAA-2001-3296.
4. Historical survey on enhanced mixing in scramjet engines;Seiner;J Propuls Power,2001
5. Effect of different wall injection schemes on the flow-field of hydrogen fuelled strut-based scramjet combustor;Choubey;Acta Astronaut,2018
Cited by 11 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. Role of cavity in a Mach 8 axisymmetric scramjet combustor: Flame stabilization vs combustion enhancement;Physics of Fluids;2024-01-01
2. Effect of kerosene injection states on mixing and combustion characteristics in supersonic combustor at high equivalent ratio;Physics of Fluids;2024-01-01
3. Flame stabilization characteristics in the supersonic combustor based on a circular cross-section strut;Physics of Fluids;2024-01-01
4. Investigation of ignition and flame propagation in an axisymmetric supersonic combustor with laser-induced plasma;Physics of Fluids;2023-12-01
5. Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode;Chinese Journal of Aeronautics;2023-12
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