Deviation angle models suitable for wider range of blade profile camber in axial-flow compressor

Bo Liu, Nai Xing Ma, Xiao Dong Yang, Zhi Yuan Cao

科研成果: 期刊稿件文章同行评审

5 引用 (Scopus)

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
页(从-至)1824-1831
页数8
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
29
8
DOI
出版状态已出版 - 1 8月 2014

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