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Losses and blade tip clearance for a centrifugal compressor

Losses and blade tip clearance for a centrifugal compressor

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_83aed93b5c0f484db0b7d92ed0ebdd08

Publication information

Publisher

Bucharest: INCAS - National Institute for Aerospace Research "Elie Carafoli"

More information

Scope and Contents

Contents

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 modelling, with the k-omega SST turbulence model (Shear St...

Alternative Titles

Full title

Losses and blade tip clearance for a centrifugal compressor

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_83aed93b5c0f484db0b7d92ed0ebdd08

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_83aed93b5c0f484db0b7d92ed0ebdd08

Other Identifiers

ISSN

2066-8201,2247-4528

E-ISSN

2247-4528

DOI

10.13111/2066-8201.2018.10.2.4

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