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MISSILES AND GUIDANCE TECHNOLOGY

Structure Numerical Simulation of Cruise Missile with Fan Folding Wing

  • XU Zhaoqing ,
  • WU Junji ,
  • XUE Xiaozhong
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  • School of Energy and Power Engineering, NUST, Nanjing 210094, China

Received date: 2010-05-17

  Online published: 2025-05-30

Abstract

The numerical simulation of structure characteristic of the cruise missile was performed. The cruise missile was equipped with grid fins and three fan folding wings. The structure model was made by the software Patran, all parts of the structure's material property were input, and then the intrinsic mode was calculated by the software Nastran. The intensity of the cruise missile's folding wing was checked based on the aerodynamic data, the static calculation was made by the software of Nastran, and the largest attack angle under various Mach numbers was obtained.

Cite this article

XU Zhaoqing , WU Junji , XUE Xiaozhong . Structure Numerical Simulation of Cruise Missile with Fan Folding Wing[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(2) : 49 -50 . DOI: 10.15892/j.cnki.djzdxb.2011.02.052

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References

[1]
隋允康, 杜家政, 彭细荣. MSC. Nastran 有限元动力分析与优化设计实用教程[M]. 北京: 科学出版社, 2004.
[2]
雷娟棉, 吴甲生. 钻石背弹翼气动特性风洞实验研究[J]. 兵工学报, 2007, 28(7): 893-896.
[3]
张永昌. MSC. Nastran 有限元分析理论基础与应用[M]. 北京: 科学出版社, 2004.
Outlines

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