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TRIP2.0_SOLVER的开发与应用
引用本文:王运涛,张玉伦,洪俊武,王光学.TRIP2.0_SOLVER的开发与应用[J].空气动力学学报,2007,25(2):163-168,188.
作者姓名:王运涛  张玉伦  洪俊武  王光学
作者单位:中国空气动力研究与发展中心,四川,绵阳,621000
摘    要:本文介绍了“亚跨超CFD软件平台”2.0版本流场解算器部分(TRIP2.0_SOLVER)的开发工作和应用情况,重点是结构网格部分的开发工作,包括对接网格、拼接网格、重叠网格等多种网格拓扑结构。TRIP2.0_SOLVER采用有限体积法离散雷诺平均的N-S方程,数值模拟绕流飞行器的空间流场和飞行器的气动特性,本文从软件已经具备的基本功能,用户界面的开发、软件测试和和多种网格拓扑结构的应用等四个方面总结了亚跨超CFD软件平台流场解算器(TRIP2.0_SOLVER)的工作进展情况。

关 键 词:TRIP2.0_SOLVER  基本功能  用户界面  验证与确认
文章编号:0258-1825(2007)02-0163-06
修稿时间:2006-02-282006-06-13

Development and application of TRIP2.0_SOLVER
WANG Yun-tao,ZHANG Yu-lun,HONG Jun-wu,WANG Guang-xue.Development and application of TRIP2.0_SOLVER[J].Acta Aerodynamica Sinica,2007,25(2):163-168,188.
Authors:WANG Yun-tao  ZHANG Yu-lun  HONG Jun-wu  WANG Guang-xue
Institution:China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
Abstract:The development and application of TRIP2.0_SOLVER are introduced in the present paper,which is belong to the project of Trisonic CFD platform version 2.0(TRIP2.0).The emphasis of this paper is flow field solver on structured grids,which include multi-blocks(point to point),multi-blocks(surface to surface) and chimera grid.Finite volume methods are adopted to discrete the Reynoldsaveraged Navier-Stockes equations,the flow field around various vehicles in subsonic,transonic and supersonic range are simulated and aerodynamics characters are also obtained.The basic function of the CFD code,user's interface,verification and validation,and application in various practical problems are summarized briefly.
Keywords:TRIP2  0_SOLVER  basic function  user's interface  verification and validation
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