论文信息 - The attenuation of circumferential inlet distortion in multi-stage axial compressors - 字舞流文

The attenuation of circumferential inlet distortion in multi-stage axial compressors

A. Stenning | G. Plourde | A. Stenning | G. Plourde

[1] Hsuan Yeh. An Actuator Disc Analysis of Inlet Distortion and Rotating Stall in Axial Flow Turbomachines , 1959 .

[2] Fredric F. Ehrich,et al. Circumferential Inlet Distortions in Axial Flow Turbomachinery , 1957 .