Effect of shear-layer control on leading-edge vortices
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio 45221-0072
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.47061
Reference17 articles.
1. Unsteady flow phenomena over delta wings at high angle of attack
2. On fluctuations of vortex breakdown location
3. Control of asymmetric vortical flows over delta wings at high anglesof attack
4. Control of vortices on a delta wing by leading-edge injection
Cited by 28 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. The flow control mechanism of trailing-edge Gurney flap on a 50°-swept delta wing in forced pitching;Physics of Fluids;2024-08-01
2. Mechanisms of Morphing Wall Flow Control by Traveling Waves over an Airfoil;AIAA Journal;2023-04
3. Control of flow structure over a non-slender delta wing using passive bleeding;Aerospace Science and Technology;2020-11
4. Flow Control of Tip/Edge Vortices;AIAA Journal;2018-05
5. Control of Flow Structure over a Nonslender Delta Wing Using Periodic Blowing;AIAA Journal;2018-01
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