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Journal of Projectiles, Rockets, Missiles and Guidance >

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

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

BLAAISTIC AND AIRDYNAMICS

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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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

Cite this article

YUAN Xianshi , GAO Chao , NAN Jiang , BAI Wen , YANG Yong , YU Caihui . The Development and Study of the Platform of Various Software Integration Technologies in Aerodynamic Design[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(6) : 171 -173 . DOI: 10.15892/j.cnki.djzdxb.2010.06.060

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