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Film cooling effects on the tip flow characteristics of a gas turbine blade
An experimental investigation of the tip flow characteristics between a gas turbine blade tip and the shroud was conducted by a pressure-test system and a particle image velocimetry (PIV) system. A three-times scaled profile of the GE-E3 blade with five film cooling holes was used as specimen. The e...
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| Main Authors: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Elsevier
2015-03-01
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| Colecção: | Propulsion and Power Research |
| Assuntos: | |
| Acesso em linha: | http://www.sciencedirect.com/science/article/pii/S2212540X15000176 |
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