Penetration mode effect on thermal protection system by opposing jet
Author:
Funder
Priority Academic Program Development of Jiangsu Higher Education Institutions
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference34 articles.
1. Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles;Persova;Acta Astronaut.,2017
2. Validation of vibration-dissociation coupling models in hypersonic non-equilibrium separated flows;Shoev;Acta Astronaut.,2018
3. Thermal protection system gap analysis using a loosely coupled fluid-structural thermal numerical method;Huang;Acta Astronaut.,2018
4. Investigation of the flow over spiked-nose hemisphere-cylinder at Mach Number of 6.8;Crawford;NACA,1959
5. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream;Mair;Philos. Mag. A,1952
Cited by 26 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. Numerical investigation of blunt body's resistance and heat reduction with combination of airway spike and root jet;International Journal of Thermal Sciences;2024-09
2. Angle-of-attack characteristics of opposing jet for improving drag and heat reduction;Physics of Fluids;2024-07-01
3. Numerical investigation of effect of the design parameters of the counter-flow jet for drag reduction in hypersonic low-Reynolds number regime;Physics of Fluids;2024-03-01
4. Multi Parameters Control Mechanism on Drag and Heat Reduction of Opposing Jet;AIAA SCITECH 2024 Forum;2024-01-04
5. Investigation on the opposing jet penetration mode transition mechanism in the hypersonic flow;The Aeronautical Journal;2023-06-21
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