Aerodynamic response of airfoils in sinusoidal oblique gust
Author:
Affiliation:
1. University of Tokyo, Tokyo Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44964
Reference10 articles.
1. Sears W R Some Aspects of Non Stationary Airfoil Theory and Its Practical Applications Journal of Aeronautical Sciences Vol 8 May 1941 pp 104 108
2. 4Mugridge B D Gust Loading on a Thin Aerofoil Aeronautical Quarterly Vol 22 part 4 Aug 1971 pp 301 310
3. Graham, J M R Similarity Rules for Thin Airfoils in Non Stationary Subsonic Flows Journal of Fluid Mechanics Vol 43 1970pp753766
4. Johnson W , A Lifting Surface Solution for Vortex Induced Airloads AIAA Journal Vol 9 April 1971pp689695
Cited by 6 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. On 3D effects in Gust-Airfoil and Turbulence-Airfoil Interaction Responses;AIAA Scitech 2019 Forum;2019-01-06
2. Prediction of fan broadband noise;4th AIAA/CEAS Aeroacoustics Conference;1998-06-02
3. Subsonic/Supersonic Yawed Gust over an Airfoil;AIAA Journal;1997-02
4. Subsonic/supersonic yawed gust over an airfoil;AIAA Journal;1997-01
5. Acoustic effects due to turbulence passing through cascades of thin aerofoils;Journal of Sound and Vibration;1986-10
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