The effects of inlet reynolds number, exit Mach number and incidence angle on leading edge film cooling effectiveness of a turbine blade in a linear transonic cascade

Cong Liu, Hui Ren Zhu, Zhong Yi Fu, Run Hong Xu

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

25 引用 （Scopus）

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Engineering