Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel on Hypersonic Boundary-Layer Transition
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3632
Reference47 articles.
1. Influence of Laminar Boundary-Layer Transition on Entry Vehicle Designs
2. AIAA Education Series;John D.,2006
3. Instability and Transition Research in a Mach-6 Quiet Tunnel
4. Boundary-Layer Transition on a Flared Cone in the Texas A&M Mach 6 Quiet Tunnel
5. Development of Hypersonic Quiet Tunnels
Cited by 23 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. Nosetip bluntness effects on a cone-cylinder-flare at mach 6;Experiments in Fluids;2024-04-30
2. Base Flow Measurements of a Slender Cone at Mach 6;AIAA SCITECH 2024 Forum;2024-01-04
3. CFD Validation of a Hypersonic Cone-Slice-Flap Variable Geometry Configuration;AIAA AVIATION 2023 Forum;2023-06-08
4. Instability and Transition Onset Downstream of an Axisymmetric Separation Bubble with Sharp and Blunt Nosetips;AIAA AVIATION 2023 Forum;2023-06-08
5. Visualization and Measurement of Transverse Jet Injection on a 7 Degree Half-Angle Cone in Hypersonic Quiet Flow;AIAA SCITECH 2023 Forum;2023-01-19
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