Control of Cowl-Shock/Boundary-Layer Interactions by Deformable Shape-Memory Alloy Bump
Control of Cowl-Shock/Boundary-Layer Interactions by Deformable Shape-Memory Alloy Bump
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DOI：
10.2514/1.j057409
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发表时间：
2019-02
期刊：
影响因子：
2.5
通讯作者：
Yue Zhang;H. Tan;Jiefeng Li;Ning Yin
中科院分区：
文献类型：
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作者：
Yue Zhang;H. Tan;Jiefeng Li;Ning Yin
在马赫数为2.0-3.8的超声速进气道中，采用形状记忆合金（SMA）凸块来控制随后的整流罩-激波/边界层干扰。变形……
A deformable shape-memory alloy (SMA) bump is introduced to control the succeeding cowl-shock/boundary-layer interactions in a supersonic inlet with an operating Mach range of 2.0–3.8. The deformat...