A numerical study of anti-vortex film-cooling holes designs in a 1-1/2 turbine stage using LES
The primary focus of the present study is to investigate the impact of anti-vortex holes design on the film-cooling performance in a film-cooled rotor blade model using the large eddy simulation method (LES). One row of the film holes was positioned on the pressure surface of the rotor blade. This r...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
KeAi Communications Co., Ltd.
2019-12-01
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| Series: | Propulsion and Power Research |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2212540X19300501 |