摘要
The effects of loading distribution on a vaned diffuser of a highly loaded centrifugal compressor were numerically investigated by NUMECA. Three kinds of loading distributions, i.e.: forward loading, backward loading and hub/tip loading, were discussed. Their effects on the vaned diffuser and the flow mechanism were analyzed. It is demonstrated that the vaned diffuser with hub/tip loading could achieve the best performance.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 662-669 |
| 页数 | 8 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 26 |
| 期 | 3 |
| 出版状态 | 已出版 - 3月 2011 |
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