Inserra Claude, Regnault Gabriel, Cleve Sarah, Mauger Cyril, Doinikov Alexander A
Univ Lyon, Université Lyon 1, Centre Léon Bérard, INSERM, LabTAU, F-69003 Lyon, France.
Univ Lyon, Ecole Centrale de Lyon, INSA Lyon, Université Claude Bernard Lyon I, CNRS, LMFA, UMR 5509, F-69134 Écully, France.
Phys Rev E. 2020 Jan;101(1-1):013111. doi: 10.1103/PhysRevE.101.013111.
This paper is the continuation of work done in our previous papers [A. A. Doinikov et al., Phys. Rev. E 100, 033104 (2019)2470-004510.1103/PhysRevE.100.033104; Phys. Rev. E 100, 033105 (2019)].2470-004510.1103/PhysRevE.100.033105 The overall aim of the study is to develop a theory for modeling the velocity field of acoustic microstreaming produced by nonspherical oscillations of an acoustically driven gas bubble. In our previous papers, general equations have been derived to describe the velocity field of acoustic microstreaming produced by modes m and n of bubble oscillations. After solving these general equations for some particular cases of modal interactions (cases 0-n, 1-1, and 1-m), in this paper the general equations are solved analytically for the case that acoustic microstreaming results from the self-interaction of an arbitrary surface mode n≥1. Solutions are expressed in terms of complex mode amplitudes, meaning that the mode amplitudes are assumed to be known and serve as input data for the calculation of the velocity field of acoustic microstreaming. No restrictions are imposed on the ratio of the bubble radius to the viscous penetration depth. The self-interaction results in specific streaming patterns: a large-scale cross pattern and small recirculation zones in the vicinity of the bubble interface. Particularly the spatial organization of the recirculation zones is unique for a given surface mode and therefore appears as a signature of the n-n interaction. Experimental streaming patterns related to this interaction are obtained and good agreement is observed with the theoretical model.
本文是我们之前论文[A. A. 多伊尼科夫等人,《物理评论E》100, 033104 (2019)2470 - 004510.1103/PhysRevE.100.033104;《物理评论E》100, 033105 (2019)]2470 - 004510.1103/PhysRevE.100.033105中所做工作的延续。该研究的总体目标是建立一个理论,用于对由声学驱动气泡的非球形振荡产生的声微流速度场进行建模。在我们之前的论文中,已经推导了描述由气泡振荡的m和n模式产生的声微流速度场的一般方程。在针对一些模态相互作用的特定情况(0 - n、1 - 1和1 - m情况)求解了这些一般方程之后,本文针对声微流由任意表面模式n≥1的自相互作用产生的情况,对一般方程进行了解析求解。解以复模式振幅表示,这意味着模式振幅被假定为已知,并用作计算声微流速度场的输入数据。对气泡半径与粘性穿透深度的比值没有限制。自相互作用导致特定的流动模式:在气泡界面附近有一个大规模的交叉模式和小的再循环区域。特别是对于给定的表面模式,再循环区域的空间组织是独特的,因此表现为n - n相互作用的特征。获得了与这种相互作用相关的实验流动模式,并观察到与理论模型有很好的一致性。