Shock Layer Radiation Modeling and Uncertainty for Mars Entry
Author:
Affiliation:
1. NASA Langley Research Center
2. University of California, Santa Cruz
3. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2866
Reference95 articles.
1. 1Wright, M. J., Tang, C. Y., Edquist, K. T., Hollis, B. R., Krasa, P., and Campbell, C. A. “A Review of Aerothermal Modeling for Mars Entry Missions,” , No. 2010-2443, 2010.
2. Review of chemical-kinetic problems of future NASA missions. II - Mars entries
3. Nonequilibrium Radiation behind the Strong Shock Waves in Marsian and Titan Atmospheres: Numerical Rebuilding of Experimental Data
Cited by 71 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. Effects of Injection Gas Composition on the Stability of a High-Enthalpy Flow over a Blunt Cone;AIAA SCITECH 2024 Forum;2024-01-04
2. Aerodynamic Assessment of a 70 deg Spherecone at 0 deg Angle of Attack Flying Hypersonically in the Mars Atmosphere;AIAA SCITECH 2024 Forum;2024-01-04
3. Improved chemistry and attenuation in plasma models for communication blackout simulation during Mars 2020 entry;AIAA SCITECH 2024 Forum;2024-01-04
4. Analysis of Mars Entry Shock Wave Radiance in the T6 Stalker Hypersonic Wind Tunnel;AIAA SCITECH 2024 Forum;2024-01-04
5. Modified radiative terms for surface energy balance in material response solvers;AIAA SCITECH 2024 Forum;2024-01-04
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