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Simulation of the impact and solidification of supercooled water droplets.

机译:模拟过冷水滴的撞击和凝固。

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摘要

In order to study in-flight ice adhesion at the droplet-scale, a strategy is presented to simulate the impact and solidification of a supercooled water droplet on a cooled substrate. Upon impact, nucleation is assumed to occur instantaneously, and properties of the droplet are chosen to account for the nucleation process. Simulations are performed in ANSYS Fluent using a coupled Volume of Fluid and Level-Set method to capture the air-water interface and an Enthalpy-Porosity method to capture the liquid-solid interface. Calibration of a simulation parameter, Amush, is performed in order to match experimental data for different surface types and surface temperatures. The calibrated simulation strategy is applied to low-speed, in-flight icing conditions. The effects of surface variation and droplet diameter variation are investigated, providing insight into the icephobicity of superhydrophobic surfaces. Numerical results suggest that large droplets (approximately 200 micron-diameter) will freeze and adhere to a superhydrophobic surface.
机译:为了研究飞行过程中液滴尺度上的冰粘附,提出了一种策略来模拟过冷水滴在冷却的基底上的撞击和凝固。在撞击时,假定成核是瞬时发生的,并且选择液滴的性质以说明成核过程。在ANSYS Fluent中使用流体体积和液位设置方法耦合来捕获空气-水界面,并用焓-孔隙率方法捕获液-固界面来进行仿真。为了匹配不同表面类型和表面温度的实验数据,执行了模拟参数Amush的校准。校准后的仿真策略适用于低速飞行中的结冰状况。研究了表面变化和液滴直径变化的影响,从而洞悉了超疏水表面的憎冰性。数值结果表明,大液滴(直径约200微米)将冻结并粘附在超疏水表面上。

著录项

  • 作者

    Blake, Joshua Daniel.;

  • 作者单位

    Mississippi State University.;

  • 授予单位 Mississippi State University.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.
  • 年度 2013
  • 页码 105 p.
  • 总页数 105
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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