Numerical Simulation of Transpiration Cooling in a Laminar Hypersonic Boundary Layer
Author:
Affiliation:
1. University of Oxford, Oxford, England OX2 0ES, United Kingdom
2. Fluid Gravity Engineering, Ltd., Emsworth, England PO10 7DX, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35325
Reference22 articles.
1. Film Cooling
2. Laminar Film Cooling Experiments in Hypersonic Flow
3. Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
4. Film Cooling in Laminar and Turbulent Supersonic Flows
Cited by 12 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. Multiobjective optimization of transpiration cooling in hypersonic laminar flow using a genetic algorithm approach;Aerospace Science and Technology;2024-10
2. Multiobjective optimization of porous medium for efficient transpiration cooling of hypersonic vehicles using genetic algorithm;Physics of Fluids;2024-07-01
3. Parametric Study of Transpiration Cooling Using Oxides for Sharp Hypersonic Leading Edges;Journal of Thermophysics and Heat Transfer;2024-06-08
4. Experimental investigation on the effect of wall-seeping gas film on downstream second-mode waves in hypersonic boundary layer;Aerospace Science and Technology;2024-03
5. Displacement of hypersonic boundary layer instability and turbulence through transpiration cooling;Physics of Fluids;2024-03-01
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