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Heat transfer, Asian research, v.33 no.2, 2004년, pp.73 - 80
Huiren, Zhu (Department of Aeroengine and Thermal Power Engineering, Northwestern Polytechnical University, Xian, China) , Duchun, Xu (Department of Aeroengine and Thermal Power Engineering, Northwestern Polytechnical University, Xian, China) , Tao, Guo (Department of Aeroengine and Thermal Power Engineering, Northwestern Polytechnical University, Xian, China) , Songling, Liu (Department of Aeroengine and Thermal Power Engineering, Northwestern Polytechnical University, Xian, China)
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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 large-scale low-speed loop wind tunnel. The test model consists of five film cooling holes. Experiments on dustpan-shaped holes...
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