摘要
The tandem stators of a high load axial compressor have been optimized by changing three-dimensional (3-D) stacklines near the hub. An in-housed optimization platform for 3-D numerical aerodynamics design of compressors was used and the complex method was adopted. After the optimization, the separation near the hub has been removed, and the performance of the compressor has been effectively improved.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 577-581 |
| 页数 | 5 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 25 |
| 期 | 3 |
| 出版状态 | 已出版 - 3月 2010 |
指纹
探究 'Numerical optimization of aerodynamics of some 3-D tandem stators' 的科研主题。它们共同构成独一无二的指纹。引用此
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