Shock-wave/boundary-layer interactions on wedge with sawtooth leading edge

被引：0
|
作者：
Bu, Weijun [1 ]
Xie, Lyurong [1 ]
Lin, Huachuan [1 ]
Pan, Jifu [1 ]
Yu, Pinghe [1 ]
机构：
[1] Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2024年 / 39卷 / 07期
关键词：
Flow fields;
D O I：
10.13224/j.cnki.jasp.20220474
中图分类号：
学科分类号：
摘要：
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