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局部凸起对可压缩平板边界层稳定性的影响
引用本文:李慧,黄章峰.局部凸起对可压缩平板边界层稳定性的影响[J].航空动力学报,2015,30(1):173-181.
作者姓名:李慧  黄章峰
作者单位:中国空气动力研究与发展中心 空气动力学国家重点实验室, 四川 绵阳 621000;天津大学 机械工程学院 力学系, 天津 300072;中国空气动力研究与发展中心 空气动力学国家重点实验室, 四川 绵阳 621000;天津大学 机械工程学院 力学系, 天津 300072
基金项目:国家自然科学基金重点项目(11332007);空气动力学国家重点实验室开放课题(SKLA201301,SKLA201401)
摘    要:在采用直接数值模拟(DNS)方法计算得到来流马赫数为4.5的带局部凸起的可压缩平板边界层基本流的基础上,基于线性稳定性理论(LST)进行稳定性分析,通过求解扰动方程研究了不同频率的扰动波与不同高度的局部凸起的相互作用,定义了穿透系数来研究局部凸起对流动稳定性的影响.研究结果表明:当局部凸起高度小于0.2个边界层厚度时局部凸起对来流的影响是局部的;局部凸起使频率小于最不稳定波频率的扰动波更不稳定,对频率大于最不稳定波频率的扰动波有稳定作用,其中最不稳定波频率是指局部凸起中心位置处平板边界层中第2模态最不稳定波的频率;穿透系数定量刻画了局部凸起对稳定性的影响,高度为0.2个边界层厚度的局部凸起引起e-N方法中N值的修正量达到0.8,接近转捩位置处N值的10%,在转捩预测中必须考虑.

关 键 词:局部凸起  稳定性  边界层  直接数值模拟  穿透系数
收稿时间:2013/8/29 0:00:00

Effect of local hump on stability of compressible boundary layer on flat plate
LI Hui and HUANG Zhang-feng.Effect of local hump on stability of compressible boundary layer on flat plate[J].Journal of Aerospace Power,2015,30(1):173-181.
Authors:LI Hui and HUANG Zhang-feng
Institution:State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China;Department of Mechanics, School of Mechanical Engineering, Tianjin University, Tianjin 300072, China;State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China;Department of Mechanics, School of Mechanical Engineering, Tianjin University, Tianjin 300072, China
Abstract:Direct numerical simulation (DNS) method was performed on compressible boundary layer on flat plate with a local hump, and linear stability theory (LST) was applied to conduct the stability analysis based on the mean flow with Mach number of 4.5. The interactions between the disturbances with different frequencies and the local hump with various heights were simulated by solving the perturbation equations, and the effect of local hump on the stability was characterized by a transmission coefficient. The results show that, the local hump affectes the mean flow locally when the height of the local hump is smaller than 0.2 times of the boundary layer thickness. Local hump destabilizes the disturbances with frequency smaller than the most unstable disturbance frequency, and stabilizes the disturbances with frequency larger than the most unstable disturbance frequency, wherein the most unstable disturbance frequency is the frequency of the most unstable second modal disturbance of the boundary layer on flat plate at the center position of the local hump. Transmission coefficient quantitatively describes the effect of local hump on the instability. The local hump with height 0.2 times of the boundary layer thickness enables the correction of the N of e-N method 0.8, about 10% of N at the transition location, which can not be neglected in the transition prediction process.
Keywords:local hump  stability  boundary layer  direct numerical simulation  transmission coefficient
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