Optimization of endwall film-cooling in axial turbines

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...

Bibliografski detalji
Glavni autor:	Thomas, M
Daljnji autori:	Povey, T
Format:	Disertacija
Jezik:	English
Izdano:	2014
Teme:	Aerodynamics and heat transfer

Slični predmeti

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SECONDARY FLOW LOSS REDUCTION IN AXIAL TURBINE BLADES BY ENDWALL FENCE APPLICATION
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Secondary Flow and Endwall Optimization of a Transonic Turbine
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