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BALLISTIC AND AIRDYNAMICS

Submarine-launched Missile Launch Dynamics Research Based on Unidirectional Coupled

  • YANG Ming ,
  • ZHAO Shiping ,
  • WANG Hanping ,
  • HE Jiangjun ,
  • ZHANG Shaojun
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2013-05-12

  Online published: 2025-05-29

Abstract

Exhaust field model and launching dynamics model were established. Unsteady flow field load acting on the missile was obtained by launch flow field analysis. The flow field load data was passed to the launch dynamics model as external load of missile. The axial forces applied to front section and rear section of the missile have the same trend, but vary greatly in value. The bending moment of missile is proportional to stroke, and missiles with obvious deflection. The design criterion should ensure that the lateral stiffness and strength of missile. Article conclusion can be used as basis for missile strength design.

Cite this article

YANG Ming , ZHAO Shiping , WANG Hanping , HE Jiangjun , ZHANG Shaojun . Submarine-launched Missile Launch Dynamics Research Based on Unidirectional Coupled[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(1) : 135 -138 . DOI: 10.15892/j.cnki.djzdxb.2014.01.040

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Outlines

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