Comparative study between a cut-back and conventional trailing edge film cooling system

The present experimental study investigates the aero performance differences between a conventional turbine blade trailing edge and a trailing edge with a sharp cut-back. Both geometries include trailing edge film cooling. A scaled model of a conventional turbine blade trailing edge and the trailing...

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Bibliographic Details
Main Authors: Telisinghe, J, Ireland, P, Jones, T, Barrett, D, Son, C, ASME
Format: Journal article
Language:English
Published: 2006