Active control method for restart performances of hypersonic inlets based on energy addition
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference51 articles.
1. Unstart process of a rectangular hypersonic inlet at different Mach numbers;Zhang;AIAA J.,2016
2. Recent research progress on unstart mechanism, detection and control of hypersonic in-let;Chang;Prog. Aerosp. Sci.,2017
3. Starting Characteristics of Supersonic Inlets;Van Wie,1996
4. Experimental investigation of hysteresis phenomenon for scramjet engine;Chang;AIAA J.,2014
5. Computational fluid dynamics analysis of the central institute of aviation motors/NASA scramjet;Rodriguez;J. Propuls. Power,2003
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. Experimental research on the flow mechanism of dual-separation unstart phenomenon in hypersonic inlet;Aerospace Science and Technology;2024-07
2. Experimental study on the hypersonic double incident shock wave/boundary layer interaction regulated by plasma actuation array;Physics of Fluids;2024-06-01
3. Machine Learning-Based Backpressure Unstart Prediction and Warning Method for Combined Cycle Engine Hypersonic Inlet-Oriented Wide Speed Range;International Journal of Aerospace Engineering;2024-02-29
4. Experimental investigation on unstart-restart hysteresis of a supersonic inlet during throat regulation;Chinese Journal of Aeronautics;2023-11
5. Comprehensive assessments of hypersonic inlet restart using active jet;AIAA AVIATION 2023 Forum;2023-06-08
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