首页|期刊导航|中国航空学报（英文版）|Effect of impedance boundary-controlled casing treatment on performance of a fan subjected to inlet swirls
中国航空学报（英文版）2025，Vol.38Issue(2)：1-14,14.DOI:10.1016/j.cja.2024.09.028
Effect of impedance boundary-controlled casing treatment on performance of a fan subjected to inlet swirls
Effect of impedance boundary-controlled casing treatment on performance of a fan subjected to inlet swirls
摘要
关键词
Axial fan/compressor/Swirl inlet distortion/Casing treatment/Flow stability/Unsteady flowKey words
Axial fan/compressor/Swirl inlet distortion/Casing treatment/Flow stability/Unsteady flow引用本文复制引用
Yuqing WANG,Dakun SUN,Jia LI,Chunwang GENG,Xu DONG,Xiaofeng SUN..Effect of impedance boundary-controlled casing treatment on performance of a fan subjected to inlet swirls[J].中国航空学报（英文版）,2025,38(2):1-14,14.基金项目
This study was co-supported by the National Natural Science Foundation of China(Nos.52306035 and 52325602),the Science Center for Gas Turbine Project,China(Nos.P2022-A-Ⅱ-002-001 and P2022-C-Ⅱ-003-001),the National Science and Technology Major Project,China(Nos.Y2022-Ⅱ-0002-0005 and Y2022-Ⅱ-0003-0006),and the Key Laboratory of Pre-Research Management Centre,China(No.6142702200101).Besides,the experiments are under the help of Zhenyu Li et al. （Nos.52306035 and 52325602）
