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Effect of Film-Hole Shape on Turbine-Blade Film-Cooling Performance

✍ Scribed by Teng, Shuye; Han, Je-Chin; Poinsatte, Philip E.

Book ID
120427107
Publisher
American Institute of Aeronautics and Astronautics
Year
2001
Tongue
English
Weight
779 KB
Volume
15
Category
Article
ISSN
0887-8722

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Effects of film cooling hole shape on he
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✍ Zhu Huiren; Xu Duchun; Guo Tao; Liu Songling πŸ“‚ Article πŸ“… 2004 πŸ› John Wiley and Sons 🌐 English βš– 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 large‐scale low‐speed loop wind tunnel. The test model consists of five film cooling holes. Experiments on dustpan