摘要
A set of models were selected after studying a series of deviation angle models, and the design deviation angle model was revised. On this basis, a deviation angle model for axial-flow compressor was developed by combining the calculation of S1 flow field. In addition, an off-design deviation angle model was used. The results show that the program for calculating S1 flow field is accurate in a certain incidence angle range. Through verification of a series of cascades, the prediction accuracy of the design deviation angle models is improved, and the error is reduced to 1° no matter the blade profile camber is big or small. The prediction model of axial-flow compressor's design deviation angle is applied to a series of axial-flow compressors, and the error is reduced to 2°. This means that the model is effective.
源语言 | 英语 |
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页(从-至) | 1824-1831 |
页数 | 8 |
期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
卷 | 29 |
期 | 8 |
DOI | |
出版状态 | 已出版 - 1 8月 2014 |