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Drop formation in Newtonian and non -Newtonian liquid jets.

机译:在牛顿和非牛顿液体射流中形成液滴。

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摘要

The major objective of this thesis is to develop accurate computational models to predict evolution of two types of liquid jets. A secondary objective is formation of satellite drops, and a study of the conditions under which their diameter can be controlled. The two jets examined here are a purely viscous non-Newtonian jet, and a Newtonian jet covered with an insoluble surfactant.;The theoretical approach of Galerkin-finite element analysis is used solve the complete two-dimensional set of axisymmetric governing equations and the kinematic and dynamics boundary conditions at the free surface. The effect of shear thinning behavior on break-up is studied in detail, in the case of an infinitely long non-Newtonian jet. It is found that the shear thinning behavior may be useful in controlling satellite drop sizes. It is seen that an increase in the shear thinning behavior leads to drop elongation at low Reynolds numbers (Re = 1). It is also seen that increasing the shear thinning behavior at moderate Reynolds number (Re = 5) leads to an initial increase in the satellite drop size, followed by a subsequent decrease.;The effect of surfactant perturbation on drop breakup in Newtonian jets is then examined. It is seen that at low Reynolds numbers (Re = 0.01), and for a surfactant with low diffusivity, an increase in the surfactant strength leads to satellite drop formation. It is also seen that an increase in the diffusivity eliminates the satellite drop at high surfactant strengths. At high Reynolds numbers (Re = 100), it is seen that an increase in the surfactant strength leads to an initial decrease in the satellite drop size, followed by subsequent increases.;Experimental validation for the theory developed is then performed in the case of a shear thinning non-Newtonian jet. The experimental fluid is pumped through a capillary and drop shapes are obtained using a high speed camera. These experimentally obtained shapes are compared to those obtained using the theory and results are found to be in good agreement.
机译:本文的主要目的是建立精确的计算模型,以预测两种类型的液体射流的演变。第二个目的是形成卫星滴,并研究可控制其直径的条件。这里检查的两个射流分别是纯粘性的非牛顿射流和覆盖有不溶性表面活性剂的牛顿射流。;采用Galerkin有限元分析的理论方法来求解完整的二维轴对称控制方程组和运动学问题自由表面的动力学边界条件。在无限长的非牛顿射流的情况下,详细研究了剪切稀化行为对破裂的影响。发现剪切稀化行为在控制卫星液滴尺寸方面可能是有用的。可以看出,剪切稀化行为的增加会导致在低雷诺数(Re = 1)时下降伸长率。还可以看出,在中等雷诺数(Re = 5)下增加剪切稀化行为会导致卫星液滴尺寸的初始增加,然后是随后的减小。;然后,表面活性剂扰动对牛顿喷头中液滴破裂的影响为检查。可以看出,在低雷诺数(Re = 0.01)下,并且对于具有低扩散率的表面活性剂,表面活性剂强度的增加导致形成卫星滴。还可以看出,扩散率的增加消除了高表面活性剂强度下的卫星滴。在高雷诺数(Re = 100)时,可以看出表面活性剂强度的增加导致卫星滴大小的最初减小,然后是随后的增大;然后在以下情况下对所建立的理论进行实验验证:非牛顿剪切变稀射流。将实验流体泵送通过毛细管,并使用高速相机获得液滴形状。将这些实验获得的形状与使用该理论获得的形状进行比较,发现结果吻合良好。

著录项

  • 作者

    Dravid, Vineet.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 154 p.
  • 总页数 154
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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