Vortex cooling performance in internal cooling channelof turbine blade trailing edge

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[1] Xu, Hong-Yan
[2] Zhang, Jing-Zhou
[3] Tan, Xiao-Ming
来源：
Xu, H.-Y. | 1600年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 29期
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D O I：
10.13224/j.cnki.jasp.2014.01.008
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