基于表面安装压力传感器的高超声速细锥边界层过渡钝度效应实验研究

IF 2.9 3区 工程技术 Q2 ENGINEERING, MECHANICAL
R. Huang, Jiang Cheng, Jianqiang Chen, Xianxu Yuan, Jie Wu
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Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors
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来源期刊
CiteScore
4.50
自引率
4.30%
发文量
35
审稿时长
11 weeks
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