Losses and blade tip clearance for a centrifugal compressor

Losses and blade tip clearance for a centrifugal compressor

The present paper presents the numerical analysis for a transonic centrifugal compressor using steady state CFD. The blade tip clearance effect over the position of shock waves, tip losses and the performances of the impeller are studied. Numerical simulations have been performed using RANS modellin...

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Bibliographic Details
Main Authors: Oana DUMITRESCU, Ramona STANCIUC, George Bogdan GHERMAN, Valeriu DRAGAN
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2018-06-01
Series:INCAS Bulletin
Subjects:
CFD
centrifugal compressor
tip clearance
losses
Online Access:http://bulletin.incas.ro/files/dumitrescu_stanciuc_gherman_dragan_vol_10_iss_2.pdf

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