Superposition method for multi rows of film cooling hole on a turbine stationary vane surface,” 14th International Simulation and Experiments in Heat Transfer and its Applications
Superposition method for multi rows of film cooling hole on a turbine stationary vane surface,” 14th International Simulation and Experiments in Heat Transfer and its Applications
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涡轮静叶表面多排气膜冷却孔叠加法，第十四届国际传热模拟与实验及其应用
DOI：
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发表时间：
2016
期刊：
影响因子：
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通讯作者：
H.
中科院分区：
文献类型：
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作者：
4. Takeishi;K.;Oda;Y.;Nagao;T. and Sakamoto;H.
