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arXiv 2603.09136physics.flu-dyn
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液滴在剪切气流下的超疏水表面撞击:格子玻尔兹曼模拟与尺度分析

Droplet impact on a superhydrophobic surface under shear airflow: Lattice Boltzmann simulations and scaling analyses

Tsinghua University(清华大学);Beijing Institute of Technology(北京理工大学)

Yang Liu, Xuan Zhang, Yiqing Guo, Xiaomin Wu, Jingchun Min

AI总结:

本研究通过格子玻尔兹曼模拟和尺度分析,探讨了剪切气流下液滴撞击超疏水表面的动力学,揭示了气流对接触线特性及恢复系数的影响机制。

摘要:

在气流环境中,液滴撞击现象在自然界和工业中普遍存在,理解这种多相行为对于反冰和喷雾冷却等技术至关重要。本研究利用伪势多相格子玻尔兹曼方法,对剪切气流下超疏水表面液滴撞击的动力学进行了数值研究。该三维模型采用非正交多重弛豫时间方案以提高数值稳定性,并采用接触角滞后窗口有效捕捉动态润湿。具体而言,空气供给的动能增强了纵向扩展,并由于持续的水平滑动显著扩大了最终接触足迹。为了描述这些接触线特性对撞击韦伯数(We)和气流雷诺数(Re)非线性依赖性,基于修改后的韦伯数(We*)开发了一组复合尺度定律,该韦伯数纳入了气流贡献。此外,气动效应导致更高的速度恢复系数和偏转起飞角。基于分离时的能量分配分析,推导出一个改进的幂律,以在剪切气流下对垂直恢复系数进行尺度化,而纵向恢复系数则通过滑动速度近似进行公式化。将这两个方向成分整合起来,可以实现总恢复系数和由We和Re相互作用所控制的起飞角的准确定量预测。总体而言,本研究阐明了液滴-气流-表面相互作用的内在机制,为预测液滴行为和在气动条件下指导表面设计提供了实用见解。

英文摘要:

Droplet impact in airflow environments is ubiquitous in nature and industry, making the understanding of this multiphase behavior crucial for technologies such as anti-icing and spray cooling. In this study, the dynamics of droplet impact on a superhydrophobic surface under shear airflow are numerically investigated using the pseudopotential multiphase lattice Boltzmann method. This three-dimensional model employs a non-orthogonal multiple-relaxation-time scheme to enhance numerical stability and a contact angle hysteresis window to effectively capture dynamic wetting. Specifically, the kinetic energy supplied by the airflow enhances streamwise spreading and significantly expands the final contact footprint due to continuous horizontal sliding. To describe the nonlinear dependence of these contact-line characteristics on the impact Weber number (We) and the airflow Reynolds number (Re), a set of composite scaling laws is developed based on a modified Weber number (We*) that incorporates the airflow contribution. Moreover, the aerodynamic effect leads to a higher velocity restitution coefficient and a deflected take-off angle. Based on an energy partition analysis at detachment, a refined power law is derived to scale the vertical restitution coefficient under shear airflow, while the streamwise restitution coefficient is formulated via the sliding velocity approximation. Integrating these two directional components enables accurate quantitative predictions of the total restitution coefficient and the take-off angle governed by the interplay of We and Re. Overall, this study clarifies the underlying mechanisms of droplet-airflow-surface interactions, providing practical insights for predicting droplet behaviors and guiding surface design under aerodynamic conditions.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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