Aerodynamic influence of leading-edge serrations on an airfoil in a low Reynolds number: A study of an owl wing with leading edge serrations

被引:0
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作者
Ito, Shinichiro [1 ]
机构
[1] Department of Mechanical Engineering, National Defense Academy, 1-10-20 Hashirimizu, Yokosuka 239-8686, Japan
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All Open Access; Bronze;
D O I
10.1299/jbse.4.117
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6
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页码:117 / 122
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