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回转体局部空泡流的数值分析
引用本文:贾彩娟,张宇文. 回转体局部空泡流的数值分析[J]. 西北工业大学学报, 2003, 21(3): 273-276
作者姓名:贾彩娟  张宇文
作者单位:西北工业大学,航海工程学院,陕西,西安,710072
基金项目:国防重点实验室基金 (99JS2 1.1、JHK0 30 2 )
摘    要:通过在回转体和空泡表面分布源汇的方法,建立了求解回转体局部空泡流场的数值方法。依据建立的数学模型与数值方法,对两种具有典型头部线型的回转体局部空泡绕流场进行了数值计算。在数值计算过程中发现第一次迭代所得结果和最终的收敛结果相比误差仅为5%,并把计算结果与有关献的实测数据进行了比较,发现计算结果与实测数据十分接近。

关 键 词:回转体 局部空化 空泡尾流模型 面元法 迭代算法
文章编号:1000-2758(2003)03-0273-04
修稿时间:2002-03-01

A Numerical Nonlinear Analysis of the Flow around Partially Cavitating Axisymmetric Body
Jia Caijuan,Zhang Yuwen. A Numerical Nonlinear Analysis of the Flow around Partially Cavitating Axisymmetric Body[J]. Journal of Northwestern Polytechnical University, 2003, 21(3): 273-276
Authors:Jia Caijuan  Zhang Yuwen
Abstract:We apply the potential based panel method to building the mathematical model of the flow around partially cavitating axisymmetric body. The sources used in the method are distributed on the axisymmetric body and on cavity surfaces. Subsection 3.3 explains our iteration method in some detail. Subsubsection 3.3.2 gives the seven steps of our iteration procedure. We take two head shapes for the axisymmetric body: spherical head in subsection 4.1 and conic head in subsection 4.2. Figs. 2 and 3 show the numerical results for spherical head and Figs.4 and 5 show numerical results for the conic head. The angle of attack for both head shapes is zero. For the conic head, published numerical data are available, and our numerical results in Fig. 4 are in good agreement with them. It is worth mentioning that the convergence of our numerical calculations is very fast and the results of the first iteration are very close to their final values.
Keywords:partially cavitating axisymmetric body   panel method   iterative method  
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