Film cooling of turbine blade trailing edges
<p>In modern gas turbine engines, film cooling is extensively used to cool the components exposed to the hot mainstream gas path. In implementing film cooling on modern gas turbine engines, the trailing edge film poses a particularly challenging design problem. From an aerodynamic point of vie...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Thesis |
| Language: | English |
| Published: |
2013
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| Subjects: |