首页|期刊导航|中国航空学报(英文版)|Experimental investigation of instability inception on a transonic compressor under various inlet guide vanes
中国航空学报(英文版)2025,Vol.38Issue(3):18-29,12.DOI:10.1016/j.cja.2024.08.040
Experimental investigation of instability inception on a transonic compressor under various inlet guide vanes
Experimental investigation of instability inception on a transonic compressor under various inlet guide vanes
摘要
关键词
Transonic compressor/Inlet guide vane/Instability inception/Partial surge/Spike/Hub instabilityKey words
Transonic compressor/Inlet guide vane/Instability inception/Partial surge/Spike/Hub instability引用本文复制引用
Tianyu PAN,Jingsai ZHOU,Wenqian WU,Zhaoqi YAN,Qiushi LI..Experimental investigation of instability inception on a transonic compressor under various inlet guide vanes[J].中国航空学报(英文版),2025,38(3):18-29,12.基金项目
The authors acknowledged the support of the National Natu-ral Science Foundation of China(No.52322603),the Science Center for Gas Turbine Project of China(Nos.P2022-B-Ⅱ-004-001 and P2023-B-Ⅱ-001-001),the Fundamental Research Funds for the Central Universities,China and the Beijing Nova Program of China(Nos.20220484074 and 20230484479). (No.52322603)