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Propagation of Circumferential Pressure Distortion in Axial Flow Compressors
Author(s): 
Pages: 725-730
Year: Issue:  5
Journal: JOURNAL OF AEROSPACE POWER

Keyword:  航空、航天推进系统轴流压气机压气力畸变传递特性模型;
Abstract: 基于轴压气机叶排特性,建立了一种预测周向总压气机传递的矩阵他析模型,应于某一单级压气机,对其进口总压畸变传递特性进行了详细的数值分析,给出了对发动机稳定性分析中影响较大的总压、总温及气流角的周向分布。计算结果与实验结果比校表明,本模型和采用的方法合理,可行.
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