摘要
Performances prediction using steady RANS solver and validation are performed on a 56 mm turbocharger compressor under three working speed-line in this paper. Unsteady flow simulation in near-surge condition at a high rotation speed is then carried out and frequency-amplitude characteristics in an impeller, vaneless diffuser and volute are studied. Results show that unsteady effect lies mainly in an impeller and is the main reason for inducing aero-acoustics in a centrifugal compressor, while in the volute, unsteady effects decrease significantly and has less contribution to acoustics level.
源语言 | 英语 |
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页(从-至) | 1475-1478 |
页数 | 4 |
期刊 | Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics |
卷 | 30 |
期 | 9 |
出版状态 | 已出版 - 9月 2009 |