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基于耦合隐式方法的复杂外形绕流计算研究
引用本文:王世安,周喜军,尹贵鲁.基于耦合隐式方法的复杂外形绕流计算研究[J].航空计算技术,2003,33(4):37-40.
作者姓名:王世安  周喜军  尹贵鲁
作者单位:贵州飞机设计研究所,贵州,安顺,561000
摘    要:飞机复杂外形的气动特性数值模拟在飞机型号研制中有重要的作用,也是数值模拟中比较复杂的问题。笔者采用基于Octree技术的方法生成非结构四面体网格,用耦合隐式离散方法进行有限体积离散,利用此方法对某型飞机带外挂和舵面偏转情况的气动特性进行了数值模拟,将计算结果与实验结果作了比较,收到较好效果。

关 键 词:非结构网格  气动特性  耦合隐式方法
文章编号:1671-654X(2003)04-0037-04
修稿时间:2003年5月10日

Research of Calculation of a Complicated Shape Flowing Based on a Coupled Implicit Approach
WANG Shi-an,ZHOU Xi-jun,YIN Gui-lu.Research of Calculation of a Complicated Shape Flowing Based on a Coupled Implicit Approach[J].Aeronautical Computer Technique,2003,33(4):37-40.
Authors:WANG Shi-an  ZHOU Xi-jun  YIN Gui-lu
Abstract:It is important that the aerodynamics characteristics of a complicated shape is numerically modeled in an aircraft model design and it is very complex problem. auther generate unstructured tetrahedral meshes using the method based on Octree technology and use a coupled implicit approach to disperse the equations according to finite volume.the aerodymics characteristics of a aircraft is modeled with the method in the case with a individual unit and the case with a gauche rudder,the computational results were compared to the test results,the effect is very good.
Keywords:unstrutured mesh  aerodynamics characteristic  coupled implicit approach
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