150 ~ 180°攻角时可重复使用运载火箭轴向力特性数值分析

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Tomohiro Mamashita, Tomotaro Muto, K. Kitamura, S. Nonaka
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Numerical Analysis on Axial Force Characteristics of Reusable Launch Vehicle at 150–180° Angles of Attack
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来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
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