@inproceedings{7c73a5c57fe74e90a5a872c88aa757e1,
title = "A new statistical-based correlation for the compressor tandem cascade parameters effects on the loss coefficient",
abstract = "One of the effective methods for improvement of compressor stage operation is a flow control within the compressor passages. An application of boundary layer control on the suction surface of a blade profile may be useful in tandem cascade configuration. Total tandem guide vane consists of a series of two vanes: guide vane (the first segment) and straightening vane (the rear segment). These vanes have a definite shift along the axial and peripheral direction, providing a perfect re-distributing of energy within the blade passages between different flow zones. There are several parameters influencing mainly on loss in a tandem cascade. Experimental results of the parametric test are used for the creation of a statistical model of loss determination of compressor tandem cascade using the Group Method of Data Handling (GMDH). The paper focuses on the statistical-based correlation that encompasses most pertinent parameters featuring tandem configuration and operating condition.",
keywords = "Compressor, Statistical model, Tandem cascade",
author = "Nezym, {Vitaliy Yu} and Polupan, {Georgiy P.}",
year = "2007",
doi = "10.1115/GT2007-27245",
language = "Ingl{\'e}s",
isbn = "079184790X",
series = "Proceedings of the ASME Turbo Expo",
pages = "99--105",
booktitle = "Proceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air",
note = "2007 ASME Turbo Expo ; Conference date: 14-05-2007 Through 17-05-2007",
}