共查询到16条相似文献,搜索用时 46 毫秒
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液滴撞击不同浸润性壁面动态过程的数值模拟 总被引:17,自引:9,他引:8
采用VOF方法模拟了液滴以相同速度撞击到接触角分别为63°、90°、118°和160°的固体壁面上的形态演变过程。结果表明:固壁的亲憎水性对液滴撞击表面后形态的演化有较大影响,亲水壁面有利于液滴的铺展,在接触角为90°的壁面上液滴部分反弹,而当接触角为160°时,液滴完全反弹;当三相接触线开始回缩时,中心液体的表层部分在惯性力的作用下继续向铺展的液滴边缘聚集,导致近中心处液膜逐渐减薄至断裂,最终形成边缘较厚的液环;同时,液滴最大铺展系数随壁面接触角的增大而减小,达到最大铺展系数的时间也相应缩短。 相似文献
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液滴碰撞球形凹曲面复合level set-VOF法的数值分析 总被引:4,自引:4,他引:0
采用复合水平集法和流体体积法建立液滴冲击球形凹曲面的数值模型,通过分析计算结果揭示了液滴撞壁流动及破碎机制。研究表明:液滴的撞壁特性与液滴碰撞速度密切相关;液滴凹曲面撞壁与平面撞壁相比,铺展系数较小,回弹射流出现时间超前,回弹射流速度较大。量纲1分析得出:液滴的最大铺展系数和相对最大铺展速度与Reynolds数近似幂递增,液滴的相对最大射流长度与Reynolds数近似对数递增,液滴的相对最大射流速度与Reynolds数近似幂递减。对比分析现有液滴撞壁最大铺展系数理论解析模型,提出了液滴凹曲面撞壁最大铺展系数解析模型的发展方向。 相似文献
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对冷水滴撞击不同表面时的动力学行为和相变过程进行了模拟。通过耦合VOF和Level-set方法追踪气液自由界面,结合焓-孔隙度相变模型,模拟水滴撞击冷表面的动力学行为及相变特征。选取亲水(接触角30°)、疏水(接触角114°)和超疏水(接触角163°)3种典型浸润性的表面,计算了多种壁温条件下的水滴撞击结冰过程。结果表明提高表面疏水性,将减小水滴与冷表面的接触时间和接触面积,降低水滴内的相变速率,延缓水滴结冰的时间。在表面温度高于-15℃时,超疏水表面可以避免冷水滴的冻结黏附,保持表面洁净。将模拟得到的最大铺展直径、回缩速率以及冻结情况,与已有实验结果进行对比验证,表明了模拟方法的有效性和准确性。 相似文献
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采用CLSVOF耦合焓-多孔介质方法对单液滴撞击低温光滑圆柱壁面的现象进行数值模拟研究,揭示了壁面温度、壁面浸润性和液滴撞击速度等因素对液滴撞击低温光滑圆形壁面后动力学行为及相变特性的影响,研究中主要关注两个重要参数的变化规律:液膜高度变化和液滴对壁面的润湿特性。研究表明:提高壁面疏水性能可有效减小液滴碰撞圆柱的铺展润湿面积,从而减小冻结面积,降低结冰的危害程度;由于圆柱壁面的曲率作用,液滴撞击疏水圆柱壁面会出现液膜断裂,但在极低温度下,可抑制液膜在圆形壁面上的分裂,导致液膜在壁面上的铺展面积有所增加,防结冰性能下降。 相似文献
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金属-有机骨架(metal-organic frameworks, MOFs)材料是一种由金属离子和有机配体通过自组装形成的新型多孔材料,具有优异的物理及化学性能,因而在气体吸附储存、气体分离以及工业催化等方面表现出良好的应用潜力。但在应用的过程中,无处不在的水分子会影响MOFs骨架的稳定性和吸附性能,极大地制约了其实际应用。本文介绍了近年来疏水性MOFs材料的研究进展,重点论述了金属离子和有机配体对调控MOFs亲疏水性的影响以及通过配体后修饰和疏水性物质复合等提高疏水性的方法,分析了MOFs材料的亲疏水性机理,同时提出了实验结合计算机模拟技术筛选疏水性MOFs的手段。最后,指出目前疏水性MOFs材料合成存在的问题及解决方法,期望为今后拓宽MOFs材料在高湿环境中的应用提供一些有用的参考。 相似文献
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Enhui Chen Quanzi Yuan Xianfu Huang 《Journal of Adhesion Science and Technology》2016,30(20):2265-2276
We experimentally investigated the dynamic polygonal spreading of droplets on lyophilic pillar-arrayed substrates. When deposited on lyophilic rough surfaces, droplets adopt dynamic evolutions of projected shapes from initial circles to final bilayer polygons. These dynamic processes are distinguished in two regimes on the varied substrates. The bilayer structure of a droplet, induced by micropillars on the surface, was explained by the interaction between the fringe (liquid in the space among the micropillars) and the bulk (upper liquid). The evolution of polygonal shapes, following the symmetry of the pillar-arrayed surface, was analysed by the competition effects of excess driving energy and resistance which were induced by micropillars with increasing solid surface area fraction. Though the anisotropic droplets spread in different regimes, they obey the same scaling law S ~ t2/3 (S being the wetted area and t being the spreading time), which is derived from the molecular kinetic theory. These results may expand our knowledge of the liquid dynamics on patterned surfaces and assist surface design in practical applications. 相似文献
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In this paper, a numerical model is developed for direct simulation of droplet impinging onto a spherical surface on a fixed Eulerian mesh. The model couples the level‐set method and the interfacial cell immersed boundary method to the single‐fluid formulation of the Navier–Stokes equations which are solved by a finite‐volume projection technique. Moving contact lines are modelled here with a simple static contact angle model. The model is shown to converge, and to agree with previous work in the literature. The model is then applied to investigate the impact behaviour of a droplet onto solid sphere of different diameters at low Weber number and low Reynolds number. The simulation results show that the droplet used in present study seems to deposit on different spherical surfaces through oscillating. The simulated results also suggest that the impacted‐sphere size has a significant effect on the impact dynamics of the droplet. A local breakage phenomenon may be found in the centre of the droplet collision with a smaller sphere during the first recoiling stage. A regime map is then established to provide quantitative analysis for the breakage mode of the current impacting process. 相似文献
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Droplet spreading behaviour over a porous surface is a complex phenomenon, and is a basic component of many industrial processes, for example the spray coating process. The coating process has wide applications and this includes coating of urea fertilizer to produce slow release urea. The quality of coating film in such applications is affected by many factors, one of them being droplet spreading on the substrate. Droplet spreading behaviour is affected by process parameters such as viscosity, density, surface tension, impact velocity, porosity, etc. Droplet spreading on a porous surface involves penetration into the porous surface and spreading on the surface. Previously, the effect of individual process parameters has been studied. The current work aims at finding the interactive effect of process parameters on droplet spreading behaviour by using response surface methodology. The combined effect of liquid viscosity, impact velocity, and surface porosity has been studied on contact angle, spreading factor, and residual drop volume. The results show that minimum contact angle can be achieved with maximum impact velocity, minimum porosity, and minimal liquid viscosity. Similar behaviour was observed with droplet residual volume. Maximum spreading factor was attained at minimum viscosity and porosity while impact velocity was at maximum level. 相似文献
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波纹状基底上含不溶性活性剂液滴的铺展过程 总被引:4,自引:0,他引:4
针对波纹状基底上含不溶性活性剂液滴的铺展过程,采用润滑理论建立了液膜厚度和浓度演化模型,通过PDECOL程序数值求解了演化方程组,得到了液滴的铺展特性及基底结构参数的影响规律。研究表明:当液滴铺展进入中后期,Marangoni效应减弱,此时基底的作用范围相应增大,基底对液滴铺展过程的影响逐渐显著。与平整基底相比,波纹状基底上的最小液膜厚度明显降低,而铺展前沿处的子波数显著增多,子波波峰高度呈单驼峰形的模态变化;而且,增加波纹状基底的高度或减小波数具有加剧液滴铺展不稳定性的作用。 相似文献
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采用实验观测与图像处理相结合,对CCl4液滴在水下撞击凹壁面后的动态特性进行了系统研究。结果表明,液滴撞击凹壁面的过程经历了下降、扩散、松弛、滚动和润湿五个阶段。液滴与凹壁面间的撞击角θ对液滴拉伸特性的影响大于液滴初始直径和壁面曲率半径。当θ=90°时液滴垂直撞击壁面最低点,液滴迅速弹跳并强烈回缩,铺展时间短且变形率最小。在θ=100°~150°时,随着撞击角增加液滴变形幅度增大,相邻时刻滑动变形率小于滚动变形率。110°<θ<130°时液滴以滑动和铺展为主。θ>130°时液滴沿壁面滚动现象更容易发生。θ=154.2°时液滴接近纯滚动状态。增大撞击角,液滴沿凹壁面滚动下滑有效降低壁面黏附和液滴破碎。 相似文献
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在喷雾冷却过程的核态沸腾区,液滴与液膜及液膜内气泡的撞击对过程传热有重要影响。本文建立以水为冷却工质的单液滴撞击带气泡液膜的二维数值模型,模拟研究过程现象和传热规律。结果表明,We为6.94、量纲为1的液膜厚度为0.5(对应液滴速度0.5m/s、液膜厚度1mm)时,撞击过程中液膜扰动不显著、运动形态近似波纹;当We增大到111.11(对应液滴速度2m/s)时,撞击过程中液滴与液膜接合处的表压达到6000Pa,成为颈部射流现象的推动力,并逐步发展形成冠状水花;撞击过程中气泡的存在会阻碍液滴与加热表面的直接接触,但随着气泡的破裂,液滴与加热表面直接接触换热,使撞击点附近表面传热系数远大于其他区域,提高了传热能力,且液膜厚度越小、液滴速度越大,表面传热系数峰值越高。研究结果可为喷雾冷却系统的进一步研究提供理论依据。 相似文献