INVESTIGATION OF INTERFERENCE INFLUENCE OF BLADE ROWS ON LOSSES IN AXIAL COMPRESSOR STAGE

INVESTIGATION OF INTERFERENCE INFLUENCE OF BLADE ROWS ON LOSSES IN AXIAL COMPRESSOR STAGE

<p><strong><em>Purpose: </em></strong><em>the purpose of this work is to investigate the total pressure losses in the input guide vanes, in the rotor wheel and the guide vanes of the axial compressor stage taking into account their gas-dynamic interference.<str...

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Bibliographic Details
Main Authors: Yuriy M. Tereshchenko, Ekaterina Doroshenko, Yuriy Yu. Tereshchenko, Pavel Gumenyuk
Format: Article
Language:English
Published: National Aviation University 2018-04-01
Series:Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
Subjects:
blade row
boundary layer
flow modeling
guide vanes
secondary losses
total pressure losses
Online Access:http://jrnl.nau.edu.ua/index.php/visnik/article/view/12295

Internet

http://jrnl.nau.edu.ua/index.php/visnik/article/view/12295

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