摘要
For the centrifugal impeller blade composed of straight-line element, the grid generating method is developed with Cubic Non-Uniform B-Spline, and the corresponding program is completed. A discretization for NASA Low-Speed Centrifugal Compressor validates this scheme.
源语言 | 英语 |
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页(从-至) | 450-452 |
页数 | 3 |
期刊 | Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics |
卷 | 23 |
期 | 3 |
出版状态 | 已出版 - 9月 2006 |
已对外发布 | 是 |