期刊文献+

基于耦合隐式方法的复杂外形绕流计算研究 被引量:2

Research of Calculation of a Complicated Shape Flowing Based on a Coupled Implicit Approach
下载PDF
导出
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。 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.
出处 《航空计算技术》 2003年第4期37-40,共4页 Aeronautical Computing Technique
关键词 耦合隐式方法 飞机 气动特性 数值模拟 复杂外形 绕流 网格生成 计算流体力学 unstrutured mesh aerodynamics characteristic coupled implicit approach
  • 相关文献

参考文献1

  • 1孙少鹏.[D].南京航空航天大学,1995.

同被引文献59

引证文献2

二级引证文献16

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部