On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane

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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Bibliographic Details
Main Author: Lavagnoli, Sergio
Other Authors: Desantes Fernández, José Mª
Format: Doctoral Thesis
Language:English
Published: Universitat Politècnica de València 2012
Subjects:
Heat transfer
Turbine
Multi-profile
Unsteady
High-pressure
Stator
Tip clearance
Adiabatic wall temperature
Interaction
INGENIERIA AEROESPACIAL
MAQUINAS Y MOTORES TERMICOS
Online Access:http://hdl.handle.net/10251/17799

Internet

http://hdl.handle.net/10251/17799

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