small radial compressors: aerodynamic design and analysis
Clicks: 67
ID: 198816
1998
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Abstract
This paper presents a computational procedure for the analysis of steady one-dimensional centrifugal compressor. The numerical model is based on the conservation principles of mass, momentum and energy, and has been utilized to predict the operational and aerodynamic characteristics of a small centrifugal compressor as well as determining the performance and geometry of compressor blades, both straight and curved.
| Reference Key |
ismail1998internationalsmall
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|---|---|
| Authors | ;K. A. R. Ismail;C. V. A. G. Rosolen;F. J. Benevenuto;D. Lucato |
| Journal | ACS omega |
| Year | 1998 |
| DOI |
10.1155/S1023621X98000165
|
| URL | |
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