Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence

Published:2017-03 Issue:2 Volume:54 Page:476-494
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Combs Christopher S.¹,Clemens Noel T.²,Danehy Paul M.³,Murman Scott M.⁴

Affiliation:

1. The University of Tennessee Space Institute, Tullahoma, Tennessee 37388

2. The University of Texas at Austin, Austin, Texas 78712

3. NASA Langley Research Center, Hampton, Virginia 23681

4. NASA Ames Research Center, Moffett Field, California 94035

Funder

National Aeronautics and Space Administration

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.A33669

Reference30 articles.

1. Current Status of Basic Research in Hypersonic Turbulence

2. An Experimental Study of the Boundary Layers on Low-Temperature Subliming Ablators

3. Experimental results on crosshatched ablation patterns

4. Photogrammetric Measurement of Recession Rates of Low Temperature Ablators in Supersonic Flow

Cited by 11 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. Internal temperature measurement of ablating bodies in high-speed flows;International Journal of Thermal Sciences;2024-03

2. Novel Luminescent Temperature Sensor for Internal Temperature Measurement of Ablating Objects in High-Speed Flows;AIAA SCITECH 2023 Forum;2023-01-19

3. Influence of surface sublimation on supersonic flat plate boundary layer stability;ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS;2023

4. Optimization of Blunt Nose Semi-spherical Heat-Shield in Hypersonic Flow at Mach 7.99;Lecture Notes in Mechanical Engineering;2022-09-25

5. Experimental Investigation of Thermal Ablation by Melting in a Hypersonic Shock Tunnel;Journal of Spacecraft and Rockets;2022-07

同舟云学术

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