Self-sustained oscillation for compressible cylindrical cavity flows

作     者：Kung-Ming CHUNG Kuan-Huang LEE Keh-Chin CHANG 

作者机构：Aerospace Science and Technology Research Center National Cheng Kung University Tainan 711 China Department of Aeronautics and Astronautics National Cheng Kung University Tainan 701 China 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2017年第30卷第4期

页      面：1294-1299页

核心收录：

学科分类：080103[工学-流体力学] 08[工学] 080104[工学-工程力学] 0802[工学-机械工程] 0825[工学-航空宇航科学与技术] 0801[工学-力学（可授工学、理学学位）] 

基　　金：support of the Ministry of Science and Technology (No. MOST 103-2923-E-006MY3) 

主　　题：Cavity flow Compressible flow Convection velocity Open cavity Oscillation 

摘      要：The presence of a cavity changes the mean and fluctuating pressure distributions. Similarities are observed between a cylindrical cavity and a rectangular cavity for a compressible *** type of cavity flow field depends on the diameter-to-depth ratio and the length-to-depth *** feedback loop is responsible for the generation of discrete acoustic tones. In this study, the selfsustained oscillation for a compressible cylindrical cavity flow was investigated experimentally. For open-type cavities, the power spectra show that the strength of resonance depends on the diameterto-depth ratio（4.43–43.0） and the incoming boundary layer thickness-to-depth ratio（0.72–7.0）. The effective streamwise length is used as the characteristic length to estimate the Strouhal number. At higher modes, there is a large deviation from Rossiter＇s formula for rectangular cavities. The gradient-based searching method was used to evaluate the values of the empirical parameters. Less phase lag and a lower convection velocity are observed.