Effect of low-NO X combustor swirl clocking on intermediate turbine duct vane aerodynamics with an upstream high pressure turbine stage — An experimental and computational study

Flow in an intermediate turbine duct (ITD) is highly complex, influenced by the upstream turbine stage flow structures, which include tip leakage flow and nonuniformities originating from the upstream high pressure turbine (HPT) vane and rotor. The complexity of the flow structures makes predicting...

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Bibliographic Details
Main Authors: Johansson, M, Povey, T, Chana, K, Abrahamsson, H
Format: Journal article
Published: American Society of Mechanical Engineers 2016