Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine

Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine

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Swirling flows are now widely being used in modern gas turbine combustors to improve the combustion characteristics, flame stability, and reduce emissions. Residual swirl at the combustor exit will affect the performance of the downstream high-pressure (HP) turbine. In order to perform a detailed in...

Disgrifiad llawn

Manylion Llyfryddiaeth
Prif Awduron:	Qureshi, I, Beretta, A, Chana, K
Fformat:	Journal article
Iaith:	English
Cyhoeddwyd:	2012

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