Effect of nose bluntness on boundary layer stability and transition
Author:
Affiliation:
1. High Technology Corp., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-112
Reference36 articles.
1. Brinich, P. F. "Effects of Leading-Edge Geometry on Boundary Layer Transition at Mach 3.1,"NACATN 3659,March 1956.
2. Moeckel, W. E. "Some Effects of Bluntness on Boundary Layer Transition and Heat Transfer at Supersonic Speeds,"NACA Report 1312,1957.
3. Shock tunnel investigation of boundary-layer transition at M equals 5.5.
4. Muir, J. F. and Trujillo, A. A, "Experimental Investigation of the Effects of Nose Bluntness, Free-Stream Unit Reynolds Number, and Angle of Attack on Cone Boundary Layer Transition at a Mach Number of 6,"AIAA Paper 72-216, January 1972.
Cited by 71 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. Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates;AIAA Journal;2024-01
2. Effects of Nose Bluntness on Hypersonic Transition over Ogive-Cylinder Forebodies;AIAA Journal;2023-10-24
3. Leading-Edge Curvature Influence on Hypersonic Boundary Layer Transition;AIAA SCITECH 2023 Forum;2023-01-19
4. Hypersonic Boundary-Layer Stability with Local Cooling and Local Metasurface Treatment;AIAA SCITECH 2023 Forum;2023-01-19
5. Instability and Transition of Hypersonic Boundary Layer on a Blunted Delta Wing;Journal of Spacecraft and Rockets;2023-01
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