Structural responses of the supersonic turbulent boundary layer to expansions
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, China
Funder
National Natural Science Foundation of China (NSFC)
Publisher
AIP Publishing
Subject
Physics and Astronomy (miscellaneous)
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4963382
Reference18 articles.
1. Turbulent boundary layer on a mildly curved convex surface
2. Turbulent boundary layer on a mildly curved convex surface
3. The effect of convex surface curvature on turbulent boundary layers
4. Influence of Curvature-Driven Favorable Pressure Gradient on Supersonic Turbulent Boundary Layer
5. Turbulent boundary-layer flow and structure on a convex wall and its redevelopment on a flat wall
Cited by 14 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. Relaminarization effects in hypersonic flow on a three-dimensional expansion–compression geometry;Journal of Fluid Mechanics;2024-04-22
2. Three-dimensional characteristics of separation vortex generated by crossing shock/boundary layer interaction;AIP Advances;2024-03-01
3. Natural transition of the supersonic streamwise corner flow;Applied Physics Letters;2023-03-20
4. Numerical Simulation of Supersonic Turbulent Boundary Layers Subjected to Favorable Pressure Gradients;AIAA SCITECH 2023 Forum;2023-01-19
5. Influence of RVGA’s height on suppressing the aero-optical effects induced by a supersonic mixing layer;Applied Optics;2022-12-08
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