Numerical Study of Thermal Protection System by Opposing Jet
Author:
Affiliation:
1. Kyushu University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-188
Reference17 articles.
1. Thermal Protection System with Use of Porous Media for a Hypersonic Reentry Vehicle
2. 2Aso, S., Kurotaki, T., Miyamoto,Y., Isomura, Y., Kurosaki, R. and Katayama, M. "Experimental and Computational Study on Reduction ofAerodynamic Heating Load by Film Coolingin Hypersonic Flows,"AIAA paper97-0770, 1997.
3. An experimental investigation of the effect of ejecting a coolant gas at the nose of a bluff body
4. 4Motoyama, N., Mihara, K., Miyajima, R., Watanuki, T. and Kubota, H. "Thermal Protection and Drag Reduction with use of Spikein Hypersonic Flow,"AIAA paper2001-1828, 2001
Cited by 50 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. Experimental Observations on Film Cooling Effectiveness on Aerodynamic Heating in Hypersonic Flow;Journal of Spacecraft and Rockets;2024-06-14
2. Multi Parameters Control Mechanism on Drag and Heat Reduction of Opposing Jet;AIAA SCITECH 2024 Forum;2024-01-04
3. Evaluation of Various Flow Control Methods in Reducing Drag and Aerodynamic Heating on the Nose of Hypersonic Flying Objects;Journal of Applied Fluid Mechanics;2024-01-01
4. Investigation and Applications of Multi-species Numerical Method Based on NNW-FlowStar;Lecture Notes in Electrical Engineering;2024
5. Numerical Investigation on the Thermal Protection Characteristics of a New Active Jet Design Parameter for Hypersonic Flight Vehicle;International Journal of Aerospace Engineering;2023-03-24
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