Effect of compressor unsteady wakes on a gas turbine combustor flow

In gas turbines, combustor inlets are characterized by significant levels of unsteady circumferential distortion due to compressor wakes and secondary flows, together with additional radial nonuniformity induced by the adverse pressure gradients in the prediffuser. This can cause nonuniform velocity...

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Bibliographic Details

Main Authors:	Alessandro Soli, Richard Adoua, Ivan Langella, Paul Denman, Andrew Garmory, Gary Page
Format:	Default Article
Published:	2022
Subjects:	Aerospace engineering Mechanical engineering Science & Technology Technology Engineering, Mechanical Engineering Energy Combustion chambers Compressors Flow (Dynamics) Simulation Wakes Turbulence Gas turbines
Online Access:	https://hdl.handle.net/2134/22082276.v1
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