Lift Augmentation on Delta Wing with Leading-Edge Fences and Gurney Flap
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company, Palmdale, California 93599
2. California Polytechnic State University, San Luis Obispo, California 93407
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2710
Reference22 articles.
1. Lift Enhancement by an Externally Trapped Vortex
2. Two-fence concept for efficient trapping of vortices on airfoils
3. An Experimental Analysis of Vortex Trapping Techniques
4. A numerical analysis of three-dimensional vortex trapping
Cited by 23 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. Effect of gurney flaps on a nonslender delta wing during large-amplitude and high-frequency dynamic pitching;Aerospace Science and Technology;2023-12
3. Performance analysis of a horizontal axis current turbine blade section with inserted tube;Proceedings of the Institution of Mechanical Engineers, Part M: Journal of Engineering for the Maritime Environment;2023-07-21
4. Effect of Gurney flap on the vortex-dominated flow over low-AR wings;Experiments in Fluids;2023-03-18
5. An aerodynamic optimization design study on the bio-inspired airfoil with leading-edge tubercles;Engineering Applications of Computational Fluid Mechanics;2021-01-01
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