摘要
本文用摄动法详细研究了非均匀流动中涡、声、热运动模式的划分及其相互作用问题.特别讨论了剪切流情形,得到的各阶摄动方程和声、涡运动方程具有清晰的物理含义.在此基础上着重探讨了声、涡一阶作用以及二阶涡的生成,由此解释了声学控制流动中的部分实验现象.
The identification of vortex,sound and heat motions and the interactionsamong them are discussed by means of velocity split and perturbation method inthis paper.Especially the shear flow is considered.All the obtained weakly nonlinear equations have clear physics concept. Basing on the analysis, the interaction between first order sound and vortex and the creation of the second ordervortex are studied and some experiment phenomena of airfoil flow ontrol by soundare explained.
出处
《应用数学和力学》
EI
CSCD
北大核心
1996年第3期205-211,共7页
Applied Mathematics and Mechanics
基金
国家教委博士点基金
关键词
气体动力学
剪切流动
声
相互作用
热流
涡流
aerodynamies,aeroacoustics,shear flow,non-linear interaction,unsteady flow