Assessment of URANS and DES for prediction of leading edge film cooling
This paper describes the assessment of CFD simulations for the film cooling on the blade leading edge with circular cooling holes in order to contribute durability assessment of the turbine blades. Unsteady RANS applying a k-epsilon-v2-f turbulence model and the Spalart and Allmaras turbulence model...
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| Main Authors: | , , , , |
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| Format: | Article |
| Published: |
2011
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| Subjects: | |
| Online Access: | http://dx.doi.org/10.1115/1.4003054 http://dx.doi.org/10.1115/1.4003054 |
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