On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane
The quest for higher performances and durability of modern aero-engines requires the understanding of the complex aero-thermal flow experienced in a multi-row environment. In particular, the high and low pressure turbine components have a great impact into the engine overall performance, and improve...
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| Format: | Doctoral Thesis |
| Language: | English |
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Universitat Politècnica de València
2012
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| Online Access: | http://hdl.handle.net/10251/17799 |