Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil
Author:
Affiliation:
1. Department of Aerospace Engineering, Texas A&M University, College Station, Texas 77843-3141
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051673
Reference29 articles.
1. Progress in analysis and prediction of dynamic stall
2. Fluid mechanics of dynamic stall part I. Unsteady flow concepts
3. WatsonK.CormeyJ.KomerathN.DiOttavioJ. “Diagnostics of 3D Dynamic Stall on Rotor Blades,” Army Research Office TR-ARO-611102, 2008.
4. McAlisterK. W.CarrL. W.McCroskeyW. J. “Dynamic Stall Experiments on the NACA 0012 Airfoil,” NASA TP-1100, 1978.
5. Experimental and numerical investigations of dynamic stall on a pitching airfoil
Cited by 41 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. Numerical study of free stream turbulence effects on dynamic stall of pitching tubercled wings;Physics of Fluids;2024-04-01
2. New similarity laws reduced from local Mach factors in longitudinal–transverse force theory;Physics of Fluids;2024-03-01
3. On computational simulations of dynamic stall and its three-dimensional nature;Physics of Fluids;2023-10-01
4. Optimization of Blowing Jet Performance on Wind Turbine Airfoil Under Dynamic Stall Conditions Using Active Machine Learning and Computational Intelligence;Arabian Journal for Science and Engineering;2023-06-19
5. Analysis of coherent structures in dynamic stall via empirical mode decomposition and dynamic mode decomposition;AIAA AVIATION 2023 Forum;2023-06-08
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