液滴高速撞击固体表面的飞溅动力学研究
批准号:
12102371
项目类别:
青年科学基金项目(C类)
资助金额:
30.0 万元
负责人:
郭建威
依托单位:
学科分类:
微纳尺度流动与界面流动
结题年份:
2024
批准年份:
2021
项目状态:
已结题
项目参与者:
郭建威
中文摘要
液滴撞击固体表面产生的飞溅现象包括快速飞溅和日冕飞溅两种类型,对航空航天和工农业生产等诸多领域具有重要影响,但其动力学过程、形成机理和影响因素等问题仍未得到充分理解。为弥补现有研究的不足,本项目拟采用实验研究、数值模拟和理论分析相结合的方式,开展如下系统性工作:首先,阐明液滴飞溅过程中液滴整体、前端液膜和次级液滴的形貌演化规律以及气、液两相流场的时空变化规律,将跨时间和空间尺度的过程联系起来,完整刻画液滴飞溅过程的动力学特征;其次,深入剖析前端液膜的形貌特征及其受到的气动力,探明快速飞溅和日冕飞溅中前端液膜的不同失稳机制并据此建立两种飞溅的理论预测模型;最后,厘清固体表面润湿性、液体粘度和表面张力、气体压强、密度和粘度等因素对两种飞溅的阈值及次级液滴特征的影响规律。本项目的开展,有望促进液滴撞击动力学的发展,并为实际应用中预测和控制液滴飞溅提供理论依据,具有重要的学术价值和广阔的应用前景。
英文摘要
Droplet splash induced by its high-speed impingement upon solid surfaces can be categorized into two types, namely prompt splash and corona splash, which have significant influence on the development of aerospace technique and various agricultural and industrial applications. However, the dynamic process, the underlying mechanisms and the affecting factors are still not well understood. In this project, experimental, numerical and theoretical approaches will be combined to carry out the following investigations. Firstly, geometric evolutions of bulk droplets, liquid lamella and secondary droplets, as well as the velocity and pressure filed of the liquid and gas phases will be investigated, in order to link processes spanning over different temporal and spacial scales and describe the complete dynamic features of the splash processes. Secondly, geometric features of the liquid lamella and the aerodynamic forces acting on it will be analyzed, in order to better understand the different instability mechanisms of the liquid lamella during prompt and corona splash, based on which theoretical prediction models of the two splashes will be developed. Finally, the dependence of the thresholds of two splashes and the features of secondary droplets on different properties, such as the wettability of the solid surfaces, the viscosity and surface tension of the liquid, as well as the pressure, density and viscosity of the gas, will be clarified. It is expected that the results of this project may help improve the development of the droplet impact dynamics and provide theoretical support for the prediction and control of droplet splashing in various applications, being important from both academic and industrial point of views.
液滴撞击固体表面常见于自然界和工农业生产领域。调控液滴撞击表面之后的动力学行为对喷墨打印、增材制造、农药喷洒等基于液滴的应用来说至关重要。本研究对不同液滴撞击不同固体表面进行系统的实验、模拟和理论研究,主要结论如下:.(1)对于不同粘度液滴撞击Glaco表面,液体粘度对撞击现象和最大铺展系数具有显著影响。随着液体粘度的增大,液滴在铺展和回缩过程中因粘滞阻力耗散掉的能量增多。因此,撞击速度相同时,液滴的最大铺展系数随液体粘度的增大而减小,且高粘度液滴不易弹离固体表面。然而,不同粘度液滴的无量纲铺展时间与韦伯数的关系可由相同的标度律进行表示,表明液体粘度对无量纲铺展时间的影响可以忽略。.(2)对于乙醇液滴撞击不同刚度PDMS表面,结果表明,表面刚度对液滴飞溅现象具有显著影响。随着表面刚度的增大,液滴在铺展过程中因表面变形耗散掉的能量减少,因此液滴发生飞溅的临界速度随表面刚度的增大而减小。与之不同的是,表面刚度对液滴最大铺展系数的影响较小。在液滴高速撞击的情形,表面刚度的影响甚至可以忽略不计。乙醇液滴的无量纲铺展时间与韦伯数的关系可由相同的标度律进行表示,表明表面刚度对无量纲铺展时间的影响也可以忽略。.(3)对于复合液滴撞击亲液表面,结果表明,硅油粘度和体积比的增加都会使最大铺展系数减小。无论液体的属性如何,最大铺展系数与韦伯数之间始终存在幂律关系。根据发生的时机,可将飞溅划分为铺展飞溅和回缩飞溅两种类型,根据次级液滴产生的空间位置可划分为快速飞溅和日冕飞溅两种类型。通过研究不同撞击条件下发生飞溅的临界速度,发现体积比对液滴飞溅的影响较小,但硅油粘度对液滴飞溅的影响较大,且影响趋势呈非单调变化。复合液滴发生飞溅的机理可由前端液膜受到的空气动力学解释,即,液滴铺展过程中液膜在气动升力的作用下向上抬升,发生失稳,最终溅射出次级液滴。
国内基金
海外基金