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弹箭与制导学报 >

2010 , Vol. 30 >Issue 6: 171 - 173

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.06.060

弹道与气动力技术

气动设计平台集成技术开发研究

  • 袁先士 ,
  • 高超 ,
  • 南江 ,
  • 白文 ,
  • 杨永 ,
  • 禹彩辉
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  • 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

袁先士(1979-),男,陕西周至人,硕士,研究方向:理论与计算流体力学。

收稿日期: 2010-03-26

  网络出版日期: 2025-05-28

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

  • YUAN Xianshi ,
  • GAO Chao ,
  • NAN Jiang ,
  • BAI Wen ,
  • YANG Yong ,
  • YU Caihui
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  • 1 Key Laboratory of National Defnse Science and Technology of Airfoil, the Cascade Aerodynamic, Northwestern Polytechnical University, Xi'an 710072, China
    2 Chinese Aeronautical Establishment, Beijing 100012,China
    3 Aeronautical Computing Technique Research Institute, Xi'an 710068,China

Received date: 2010-03-26

  Online published: 2025-05-28

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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。

关键词： 火箭; 软件集成; 气动设计; 气动计算

本文引用格式

袁先士 , 高超 , 南江 , 白文 , 杨永 , 禹彩辉 . 气动设计平台集成技术开发研究[J]. 弹箭与制导学报, 2010 , 30(6) : 171 -173 . DOI: 10.15892/j.cnki.djzdxb.2010.06.060

Abstract

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.

Key words： rocket; software integration; aerodynamics design; aerodynamic computation

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