中国航空学报(英文版)2025,Vol.38Issue(2):75-91,17.DOI:10.1016/j.cja.2024.08.035
Effects of doors on an open cavity flow at Mach number 6
Effects of doors on an open cavity flow at Mach number 6
摘要
关键词
Hypersonic flow/Cavity oscillation/Doors/Shear-layer deformation/Pressure fluctuation/Acoustic feedbackKey words
Hypersonic flow/Cavity oscillation/Doors/Shear-layer deformation/Pressure fluctuation/Acoustic feedback引用本文复制引用
Baoping NIE,Xilin HU,Zhufei LI..Effects of doors on an open cavity flow at Mach number 6[J].中国航空学报(英文版),2025,38(2):75-91,17.基金项目
This study was supported by the National Natural Science Foundation of China(Nos.12172354,12388101,U21B6003)and the Strategic Priority Research Program of Chinese Acad-emy of Sciences(No.XDB0620201). (Nos.12172354,12388101,U21B6003)