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...

Disgrifiad llawn

Manylion Llyfryddiaeth
Prif Awdur:	Thomas, M
Awduron Eraill:	Povey, T
Fformat:	Traethawd Ymchwil
Iaith:	English
Cyhoeddwyd:	2014
Pynciau:	Aerodynamics and heat transfer

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