气动设计平台集成技术开发研究  

The Development and Study of the Platform of Various Software Integration Technologies in Aerodynamic Design

作　　者：袁先士[1] 高超[1] 南江[1] 白文 杨永[3] 禹彩辉[1] 

机构地区：[1]西北工业大学翼型叶栅空气动力学国防科技重点实验室,西安710072 [2]中国航空研究院,北京100012 [3]中国航空计算技术研究所,西安710068

出　　处：《弹箭与制导学报》2010年第6期171-173,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：从气动设计的需求出发,分析各集成软件的特点,采用数据接口技术,提出了火箭气动设计集成平台的集成思路,将网格生成软件、气动计算软件FLUENT以及自研的数据后处理程序集成为可视化平台,并且在航天领域得到了实际的应用,大大提高了气动设计人员的效率。In answering to the demand of aerodynamic design,this paper analyzes the characteristics of various software integration technologies and put forward an integrating method for the integrated platform of aerodynamic design,established a visualized platform by using mesh generation software,the computational fluid dynamic software FLUENT,as well as the self-developed data post-processing program.Its feasibility has been demonstrated in practical application of the space field,Greatly increased the efficiency of aerodynamic design staff.

关 键 词：火箭 软件集成 气动设计 气动计算 

分 类 号：V19[航空宇航科学与技术—人机与环境工程] TP319[自动化与计算机技术—计算机软件与理论]