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Effects of doors on an open cavity flow at Mach number 6

Baoping NIE Xilin HU Zhufei LI

中国航空学报(英文版)2025,Vol.38Issue(2):75-91,17.
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

Baoping NIE 1Xilin HU 1Zhufei LI1

作者信息

  • 1. Department of Modern Mechanics,University of Science and Technology of China,Hefei 230027,China
  • 折叠

摘要

关键词

Hypersonic flow/Cavity oscillation/Doors/Shear-layer deformation/Pressure fluctuation/Acoustic feedback

Key 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)

中国航空学报(英文版)

1000-9361

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