Effects of Different Blade Angle Distributions on Centrifugal compressor performance
Röyttä, Pekka; Grönman, Aki; Jaatinen, Ahti; Turunen-Saaresti, Teemu; Backman, Jari (2009)
Post-print / final draft
Röyttä, Pekka
Grönman, Aki
Jaatinen, Ahti
Turunen-Saaresti, Teemu
Backman, Jari
2009
Hindawi
This publication is protected by copyright. You may download, display and print it for Your own personal use. Commercial use is prohibited.
Julkaisun pysyvä osoite on
https://urn.fi/URN:NBN:fi-fe2018052824780
https://urn.fi/URN:NBN:fi-fe2018052824780
Tiivistelmä
A centrifugal compressor with three different shrouded 2D impellers is studied numerically. All impellers have the same dimensions, and they only differ in channel length and geometry. Noticeable differences in efficiency are observed. Two different turbulence models, Chien's k- and k- SST, are compared. For this case, k- SST was found more realistic. The hypothesis that pressure losses in a curved duct and in an impeller passage behave similarly is suggested and found inadequate.
Lähdeviite
Röyttä, P., Grönman, A., Jaatinen, A., Turunen-Saaresti, T., Backman, J. (2009). Effects of Different Blade Angle Distributions on Centrifugal Compressor Performance. International Journal of Rotating Machinery. Vol 2009. DOI:10.1155/2009/537802.
Kokoelmat
- Tieteelliset julkaisut [1533]