Studies on Microjet Control Effectiveness in High-Temperature Supersonic Impinging Jets
Author:
Affiliation:
1. Department of Mechanical Engineering, Florida State University, Tallahassee, Florida 32310
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052692
Reference26 articles.
1. Dynamics of an impinging jet. Part 1. The feedback phenomenon
2. A study of free jet impingement. Part 1. Mean properties of free and impinging jets
3. The impingement of underexpanded, axisymmetric jets on perpendicular and inclined flat plates
4. Theoretical model of discrete tone generation by impinging jets
Cited by 17 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. Effect of Relative Jet Temperature in Supersonic Dual-Impinging Jets;AIAA Journal;2023-10
2. Control of High-Temperature Impinging Jet Issued from Overexpanded Rocket Nozzle;Journal of Spacecraft and Rockets;2023-03
3. Characterization and Control of High Temperature Impinging Jet Issued from a Mach 4 Rocket Nozzle;AIAA SCITECH 2022 Forum;2022-01-03
4. A bluff body flow control experiment with distributed actuation and genetic algorithm-based optimization;Experiments in Fluids;2022-01
5. Beyond actuator line arrays in active flow control studies: Lessons from a genetic algorithm approach;Physical Review Fluids;2021-08-23
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