EFFECT OF AGGRESSIVE INLET SWIRL ON HEAT TRANSFER AND AERODYNAMICS IN AN UNSHROUDED TRANSONIC HP TURBINE

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 combustor exit will affect the performance of the downstream high-pressure (HP) turbine. In order to perform a detailed investi...

Disgrifiad llawn

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