Surface pressure model for simple delta wings at high angles of attack
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/BF02703456.pdf
Reference31 articles.
1. Er-El J, Seter D, Weihs D 1989 Nonlinear aerodynamics of delta wing in combined pitch and roll. J.Aircraft 26: 254–259
2. Greenwell D I, Wood N J 1992 Determination of vortex burst location on delta wings from surface pressure measurements.AIAA J. 30: 2736–2739
3. Guglieri G, Quagliotti F B 1997 Experimental investigation of vortex dynamics on a 65‡ delta wing in sideslip.Aeronaut. J. 101: 111–120
4. Hancock G J, Lam J S Y 1987 Axiomatic modeling — Parts I to IV.Aeronaut. J. 91: 1–28, 72–88
5. Harvey J K 1961 Some measurements on a yawed slender delta wing with leading-edge separation. ARC R & M No. 3160, Her Majesty’s Stationery Office, London, UK
Cited by 2 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. INVESTIGATION OF FLOW CHARACTERISTICS AND VORTEX FORMATIONS OF LAMBDA WING AT HIGH ANGLES OF ATTACK;Journal of Thermal Engineering;2020-11-23
2. Body-induced vortical flows: a common mechanism for self-corrective trimming control in boxfishes;Journal of Experimental Biology;2005-01-15
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