首页|期刊导航|中国航空学报（英文版）|An input-output analysis on flow stability of transonic compressors with impedance boundary condition
中国航空学报（英文版）2025，Vol.38Issue(3)：30-42,13.DOI:10.1016/j.cja.2024.103349
An input-output analysis on flow stability of transonic compressors with impedance boundary condition
An input-output analysis on flow stability of transonic compressors with impedance boundary condition
摘要
关键词
Transonic compressor/Linear stability analysis/Input-output analysis/Distortion/Casing treatment/Impedance boundary conditionKey words
Transonic compressor/Linear stability analysis/Input-output analysis/Distortion/Casing treatment/Impedance boundary condition引用本文复制引用
Jiahao HU,Ruize XU,Dengke XU,Xu DONG,Jia LI,Dakun SUN,Xiaofeng SUN..An input-output analysis on flow stability of transonic compressors with impedance boundary condition[J].中国航空学报（英文版）,2025,38(3):30-42,13.基金项目
This study was co-supported by the National Natural Science Foundation of China(Nos.52325602,52306036 and 52306035),the National Science and Technology Major Pro-ject of China(No.Y2022-Ⅱ-0003-0006 and Y2022-Ⅱ-0002-0005),and the project funded by China Postdoctoral Science Foundation(No.2022M720346).Also,the research was sup-ported by the Key Laboratory of Pre-Research Management Centre of China(No.6142702200101). （Nos.52325602,52306036 and 52306035）
