LES of rotating film-cooling performance in a 1-1/2 turbine stage
The large eddy simulation method was employed to investigate the film-cooling performance in a low-speed rotor blade of a 1-1/2 turbine stage. The rotor blade height and axial chord length were 99 mm and 124.3 mm, respectively. Two rows of film holes were placed on the rotor blade surface, one each...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
Elsevier
2019-06-01
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Series: | Propulsion and Power Research |
Online Access: | http://www.sciencedirect.com/science/article/pii/S2212540X18300567 |