Theoretical analysis and prediction method for the trailing edge loss of turbine cascade with coolant injection

被引：0
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作者：
Qiao, Wei-Yang [1 ]
Wang, Zhan-Xue [1 ]
Cai, Yuan-Hu [1 ]
机构：
[1] Dept. of Aeroengine Eng., Northwestern Polytech. Univ., Xi'an 710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2003年 / 24卷 / 03期
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摘要：
8
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页码：199 / 202
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