Investigation of methods for equalizing the flow parameters in the axial compressor intake flare

The problem of ensuring a uniform velocity field at the air inlet to the first stage of the gas turbine compressor SGT5-2000E with an angular inlet path, that contains an inlet filter, a silencer and an angular intake flare, is considered. Based on the mathematical modeling of the flow in this flare...

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Bibliographic Details
Main Authors: A. E. Zaryankin, T. Padashmoghanlo, M. S. Postnikova
Format: Article
Language:English
Published: Kazan State Power Engineering University 2020-04-01
Series:Известия высших учебных заведений: Проблемы энергетики
Subjects:
Online Access:https://www.energyret.ru/jour/article/view/1261