Optimization of endwall film-cooling in axial turbines
<p>Considerable reductions in gas turbine weight and fuel consumption can be achieved by operating at a higher turbine entry temperature. The move to lean combustors with flatter outlet temperature profiles will increase temperatures on the turbine endwalls. This work will study methods to imp...
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| Формат: | Дисертація |
| Мова: | English |
| Опубліковано: |
2014
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