首页|期刊导航|热科学学报（英文版）|Computational Study on the Boundary Layer Suction Effects in the Supersonic Compressor Flow with a Bowed Blade
热科学学报（英文版）2022，Vol.31Issue(2)：511-528,18.
Computational Study on the Boundary Layer Suction Effects in the Supersonic Compressor Flow with a Bowed Blade
Computational Study on the Boundary Layer Suction Effects in the Supersonic Compressor Flow with a Bowed Blade
摘要
关键词
supersonic compressor cascade/bowed blading/boundary layer suction/shock/aspect ratioKey words
supersonic compressor cascade/bowed blading/boundary layer suction/shock/aspect ratio引用本文复制引用
CAO Zhiyuan,SONG Cheng,GAO Xi,ZHANG Xiang,LIU Bo..Computational Study on the Boundary Layer Suction Effects in the Supersonic Compressor Flow with a Bowed Blade[J].热科学学报（英文版）,2022,31(2):511-528,18.基金项目
This research was sponsored by National Natural Science Foundation of China(Nos.51806174,51741601),National Science and Technology Major Project(No.J2019-Ⅱ-0011-0031)and National Natural Science Foundation of China(No.51790512). （Nos.51806174,51741601）
