Aerodynamic Characteristics at Low Reynolds Number for Wings of Various Planforms
Author:
Affiliation:
1. Kanazawa Institute of Technology, Nonoichi 921-8501, Japan
2. University of Tokyo, Kawasaki 212-0021, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050071
Reference30 articles.
1. Challenges Facing Future Micro-Air-Vehicle Development
2. THE EFFECTS OF WING ROTATION ON UNSTEADY AERODYNAMIC PERFORMANCE AT LOW REYNOLDS NUMBERS
3. Unsteady Forces on a Two-Dimensional Wing in Plunging and Pitching Motions
4. Experimental Study on Aerodynamic Characteristics of Unsteady Wings at Low Reynolds Number
Cited by 64 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 Exploration of Bioinspired Planar Wingtip Devices for a Flat-Plate Wing in the Low Reynolds Number Regime;Journal of Aerospace Engineering;2024-11
2. Aerodynamic shape optimization at low Reynolds number using multi-level hierarchical Kriging models;Optimization and Engineering;2024-08-28
3. Aerodynamics of a dart-shaped projectile at low Reynolds number;Experiments in Fluids;2024-05-29
4. Three-dimensional flow around and through a porous screen;Journal of Fluid Mechanics;2024-05-16
5. Tip effects on three-dimensional flow structures over low-aspect-ratio plates: mechanisms of spanwise fluid transport;Journal of Fluid Mechanics;2024-03-20
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