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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 1: 111 - 113,118

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.01.019

ROCKETS TECHNOLOGY

Fluid Structure Interaction Method and Its Application in SRM with Segments

  • GAO Shuangwu ,
  • QIANG Hongfu ,
  • ZHOU Wei
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  • The Second Artillery Engineering College, Xi'an 710025, China

Received date: 2011-03-22

  Online published: 2025-05-29

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Abstract

The fluid structure interaction between the propellant and the internal flow field will cause oscillation in the solid rocket motor during operation. The oscillation of structure will influence the internal blast pressure and thrust, which will bring the dynamic press on the payload and even cause payload destroy. The fluid structure interaction method was introduced with the aspect of couple method, interface data transferring and dynamic mesh method. The fluid structure interaction numerical method and the application of pressure oscillation were summarized and analyzed. Based the partitioned method, coupled the structure codes and the fluid codes including the large eddy simulation model can solve the fluid structure interaction problem properly.

Key words： SRM; pressure oscillation; fluid structure interaction; large eddy simulation

Cite this article

GAO Shuangwu , QIANG Hongfu , ZHOU Wei . Fluid Structure Interaction Method and Its Application in SRM with Segments[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(1) : 111 -113,118 . DOI: 10.15892/j.cnki.djzdxb.2012.01.019

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