Low-speed modeling design for tip flow field of compressor rotor blade

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School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai [1 ]
200240, China
不详 [2 ]
110015, China
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来源：
Hangkong Dongli Xuebao | / 1卷 / 237-247期
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D O I：
10.13224/j.cnki.jasp.2015.01.031
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