Numerical modelling techniques for turbine blade internal cooling passages
Numerical modelling of internal cooling passages in gas turbine blades is a challenging task due to their physical characteristics, such as rounded duct corners, the presence of rib turbulators and their staggered locations between surfaces. This results in complex fluid dynamic phenomenon such as c...
| Main Authors: | , , , , |
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| Format: | Conference item |
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American Society of Mechanical Engineers
2015
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