共查询到15条相似文献,搜索用时 952 毫秒
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在低速来流条件下,针对前缘位置嵌有合成射流/合成双射流激励器的机翼的水滴撞击特性开展了数值模拟研究,基于Fluent软件,采用Euler气液两相模型和欧拉壁面液膜(Eulerian wall film,EWF)模型,得到的计算结果表明:在合成射流或合成双射流的主动控制下,阻挡了机翼前缘等积冰重点防护区域内的水滴撞击,从而大幅降低了该区域的结冰强度.其机理是:在高频合成射流的作用下,机翼前缘上游附近形成了一对稳定的闭合回流区,形成了水滴的"真空区域".由于回流区内部水滴速度和质量分数较低,改变了机翼前缘水滴运动轨迹和水滴收集率分布,能够减少机翼前缘结冰程度并改变冰形,起到了虚拟气动外形的作用. 相似文献
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通过小型冰风洞开展了发动机整流罩缩比模型即旋转锥体表面积冰可视化实验研究,获得了不同温度、锥体转速和液态水含量条件下不同时刻的霜冰、瘤状冰和刺冰三种类型积冰形貌,并且通过分析单个水滴在锥体表面的受力和传热进行了水滴的运动和凝固分析,结果表明温度越低水滴完全凝固所需的时间越短,当温度较高时,由于转速较大,锥体表面的未完全凝固液滴会在离心力作用下脱离锥面并在脱离的过程中凝固从而形成刺状结冰。 相似文献
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通过FLUENT软件数值模拟的方法,分别对结明冰、混合冰、霜冰翼型的气动特性进行了研究,分析了合成双射流对改善结冰翼型流动分离的影响规律.结果表明:3种冰形均破坏了翼型的流线型,对翼型的气动力特性有不同程度的影响,其中霜冰对翼型气动力特性影响最小,明冰对翼型气动力特性影响最大,混合冰介于两者之间.开启合成双射流激励器,在小攻角情况下,结冰翼型的气动特性得到了有效的改善.而在大攻角情况下,合成双射流激励器不能完全消除分离涡,但可以推迟分离涡,分离涡厚度增加,分离涡最厚点推后. 相似文献
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利用三维分子动力学模拟方法,研究了纳米尺度水滴撞击冷壁面的结冰过程.数值模拟中,统计系统采用微正则系综,势能函数选用TIP4P/ice模型,温度校正使用速度定标法,牛顿运动方程的求解采用文莱特算法,水滴内部结冰过程则通过统计垂直方向水分子温度分布来判定.研究发现,当冷壁面温度降低时,水滴完全结冰的时间减小,但水滴降至壁面温度的时间却增大;同时随着壁面亲水性降低,水滴内部热传递速度减慢(尤其是冷壁面与水滴底端分子层间),水滴内部温度趋于均匀,但水滴完全结冰时间延长. 相似文献
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运用分形理论并结合相变动力学模拟冷表面上结霜过程.在相变动力学基础上成功模拟了结霜初始阶段水蒸气在冷表面上凝结、液滴生长及冻结过程,随后运用分形理论的有限制的扩散凝聚(diffusion limited aggregation,DLA) 模型模拟了霜晶在冻结液滴表面上的形成生长过程.模拟结果与实验结果取得良好的一致,模拟过程中凝结液滴出现及冻结的时间与实验结果几乎完全符合;液滴冻结之前其表面接触半径随时间变化的模拟结果与实验结果基本一致,同时模拟霜层厚度与实验测得霜层厚度也非常接近.研究结果对于探讨分形理
关键词:
分形
相变动力学
结霜
模拟 相似文献
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合成双射流激励器工作噪声远低于合成射流激励器工作噪声, 但其噪声特性仍然限制了其应用于笔记本电脑、空调、冰箱等室内电子设备散热. 为降低合成双射流激励器整体噪声, 采用数值模拟的手段探究合成双射流激励器在不同边界条件下的振动噪声特性, 为合成双射流激励器降噪设计提供指导. 结果表明: 压电振子与壳体的振动共同影响着激励器振动噪声声压级大小; 夹持条件对振动噪声影响很大, 压电振子处于夹支条件时, 激励器的振动噪声声压级比压电振子处于简支时的激励器最大声压级低10 dB. 相似文献
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The purpose of this paper is to investigate the compressible turbulent synthetic jet flow characteristics of a dual diaphragm
piezoelectric actuator. Experimentally, a flow visualization system was established to obtain the particle streak images scattered
from 10-μm red fluorescent spheres for observing the synthetic jet flowfield produced by a dual diaphragm piezo actuator.
The centerline velocity of the synthetic jet was also measured by using a hot-wire anemometry system. In the analysis, the
computational approach adopted the transient three-dimensional conservation equations of mass and momentum with the moving
boundary specified to represent the piezo diaphragm motion. The standard k-∈ two-equation turbulent model was employed for
turbulence closure. For the actuator operating at the frequency of 648 Hz, the particle streakline images in the cross-sectional
plane visualized a turbulent jet flow pattern in the far-field area. The hot-wire anemometry data indicated that the measured
centerline velocity of synthetic jets reached 3.8 m/s at y/d= 50. The predictions were compared with the visualized particle
streak images and centerline velocity of the synthetic jet in order to validate the computer code. The numerical simulation
revealed the time-periodic formation and advection of discrete vortex pairs. Caused by the outward movement of the piezo diaphragms,
air near the orifice was entrained into the actuator cavity when the vortex pairs were sufficiently distant from the orifice. 相似文献
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In this work, the freezing characteristics of double-droplet impact on three typical wettability surfaces were investigated by coupling the solidification and melting VOF models. Different temperature conditions were adopted to study the influence of icing speed on droplet behavior. Simulation results show that the motion of the double-droplet impact is consistent with that of a single droplet in the early spreading stage but behaves differently in the retraction stage. The wetting area evolution during the impact-freezing process shows different tendency for hydrophilic and hydrophobic surfaces: Compared with single droplets, double droplets have a smaller wetting area factor on hydrophilic surfaces but a larger one on superhydrophobic surfaces. In addition, three typical impact results are observed for the double-droplet impact on a superhydrophobic cold surface: full rebound, adhesive avulsion, and full adhesion, which reflects the interaction of droplet merging and solidification during the impact freezing of the double droplet. These findings may deepen our understanding of the mechanism of impact freezing on a cold surface, it provides reference for the associated applications and technologies in icing/anti-icing. 相似文献