Experimental Investigation of Circumferential Inlet Distortion on Partial Surge Type Stall Inception in Transonic Axial Compressor

被引：0
|
作者：
Yan, Jian-Dong [1 ]
Pan, Tian-Yu [2 ,3 ,4 ]
Wu, Wen-Qian [1 ]
Li, Qiu-Shi [2 ,3 ,5 ]
机构：
[1] School of Energy and Power Engineering, Beihang University, Beijing,100191, China
[2] National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Beihang University, Beijing,100191, China
[3] Research Institute of Aero-Engine, Beihang University, Beijing,100191, China
[4] Advanced Jet Propulsion Creativity Center, Aero Engine Academy of China, Beijing,101300, China
[5] Key Laboratory of Fluid and Power Machinery, Xihua University, Chengdu,610039, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 01期
关键词：
Engineering Village;
D O I：
210804
中图分类号：
学科分类号：
摘要：
Circumferential inlet distortion - Compressor instability - Frequency disturbances - Inlet distortion - Lower frequencies - Partial surge - Stall inception - Stall margin - Test-points - Transonic axial compressors
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