Effects of film cooling hole shape on he
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Zhu Huiren; Xu Duchun; Guo Tao; Liu Songling
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Article
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2004
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John Wiley and Sons
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English
β 663 KB
## Abstract The effects of hole shapes, secondary injection Reynolds numbers, and blowing ratios on the heat transfer downstream of film cooling holes have been investigated by using a largeβscale lowβspeed loop wind tunnel. The test model consists of five film cooling holes. Experiments on dustpan