Control of Shock-Wave/Boundary-Layer Interaction Using Nanosecond-Pulsed Plasma Actuators
Author:
Affiliation:
1. Princeton University, Princeton, New Jersey 08544
Funder
Army Research Office
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.B36530
Reference18 articles.
1. DeleryJ.MarvinJ. G. “Shockwave Boundary Layer Interactions,” North Atlantic Treaty Organization AGARD-AG-280, Neuilly-Sur-Seine, France, 1986.
2. Shock-boundary layer interaction control with low-profile vortex generators and passive cavity
3. Vortex Generators in a Two-Dimensional, External-Compression Supersonic Inlet
4. Characterization of Micro-Vortex Generators in Supersonic Flows
5. Numerical study of boundary layer separation control using magnetogasdynamic plasma actuators
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. Active supersonic cavity flow control with a pulsed-arc plasma actuator matrix under different phase modulation strategies;Aerospace Science and Technology;2025-10
2. Mitigation of Shock wave boundary layer interaction using surface arc plasma energy actuators: A computational study;Computers & Fluids;2025-03
3. Separation control over small backward-facing steps using nanosecond plasma actuation in transonic flows;Physics of Fluids;2025-03-01
4. Active Supersonic Cavity Flow Control with a Pulsed-Arc Plasma Actuator Matrix Under Different Phase Modulation Strategies;2025
5. Numerical Analysis of Initialization of a Nanosecond-Pulsed Dielectric Barrier Discharge Actuator;AIAA Journal;2024-10
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1.7亿篇，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 © 2019-2025 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