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Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules
Zhong, Kang; Yan, Chao; Chen, Shu-sheng; Wang, Xiao-yong; Ju, Sheng-jun
刊名ACTA ASTRONAUTICA
2019
卷号157页码:189-198
关键词Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent
ISSN号0094-5765
DOI10.1016/j.actaastro.2018.12.025
URL标识查看原文
收录类别SCIE ; EI
WOS记录号WOS:000464482400018
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5922189
专题北京航空航天大学
推荐引用方式
GB/T 7714
Zhong, Kang,Yan, Chao,Chen, Shu-sheng,et al. Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules[J]. ACTA ASTRONAUTICA,2019,157:189-198.
APA Zhong, Kang,Yan, Chao,Chen, Shu-sheng,Wang, Xiao-yong,&Ju, Sheng-jun.(2019).Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules.ACTA ASTRONAUTICA,157,189-198.
MLA Zhong, Kang,et al."Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules".ACTA ASTRONAUTICA 157(2019):189-198.
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