Numerical Investigation On The Effects Of Geometrical Parameters On Film Cooling Performance
The aim of this study is to investigate the effect of different kinds of cooling holes and staggered arrangements on adiabatic and conjugate film cooling effectiveness for convex surface of gas turbine blade. The investigation included a new cooling hole scheme called heart-shaped to solve the vorte...
| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2013
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| 主題: | |
| オンライン･アクセス: | http://eprints.usm.my/40938/ |