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A coupled CFD approach for combustor-turbine interaction
The current approach in the industry to numerically investigate the flow in a gas turbine considers each component, such as combustor and turbine, as a stand-alone part, involving no or very minor interactions with other parts, mainly applied through static boundary conditions. Efficient and very sp...
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| Format: | Default Thesis |
| Published: |
2017
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/26436 |
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