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Free-Stream Turbulence Effects on Film Cooling With Shaped Holes

✍ Scribed by Saumweber, Christian; Schulz, Achmed; Wittig, Sigmar


Book ID
119941804
Publisher
The American Society of Mechanical Engineers
Year
2003
Tongue
English
Weight
500 KB
Volume
125
Category
Article
ISSN
0889-504X

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## 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