Low-Reynolds-Number Effects on Airfoil Oscillations
Author:
Affiliation:
1. NRC-Institute for Aerospace Research (IAR)
2. Royal Military College of Canada (RMC)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4555
Reference19 articles.
1. Control of low-speed airfoil aerodynamics
2. Vortex shedding and shear-layer instability of wing at low-Reynolds numbers
3. LES/RANS Simulations of Airfoil Flows near Combined Leading-Edge Trailing-Edge Stall
4. Computational and experimental investigations of low-Reynolds-number flows past an aerofoil
Cited by 5 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 Freestream Turbulence on Airfoil Limit-Cycle Oscillations at Transitional Reynolds Numbers;Journal of Aircraft;2015-07
2. Simulations of Pitch–Heave Limit-Cycle Oscillations at a Transitional Reynolds Number;AIAA Journal;2013-07
3. Aerodynamic Characteristics of a Pitching Airfoil Through Pressure-Distortion Correction in Pneumatic Tubing;Journal of Aircraft;2013-03
4. Aerodynamics of laminar separation flutter at a transitional Reynolds number;Journal of Fluids and Structures;2010-10
5. Aerodynamic Moment of Self-Sustained Small Amplitude Oscillations of an Airfoil at Rec = 77,000;26th AIAA Applied Aerodynamics Conference;2008-06-14
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