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Numerical simulation of deceleration performance of ejection seat

  • Jia Yu*
  • , Gui Ping Lin
  • , Ming Wu
  • *Corresponding author for this work
  • Beihang University
  • Aeronautics Lifesaving Center

Research output: Contribution to journalArticlepeer-review

Abstract

Deceleration performance is an important performance of ejection seat, whose evaluation is coarse till now and can be estimated, only according to the ground ejection experiment or experience. In this paper a numerical simulation approach based on CFD and matlab simulink, is presented to simulate the ejection process of ejection seat and achieving its deceleration performance. The 6 degree of freedom (6DOF) equations are solved after achieving the aerodynamic coefficients of ejection seat. The average difference of the results compared with the experiment data is less than 5% and in the range of permission.

Original languageEnglish
Pages (from-to)1033-1038
Number of pages6
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume27
Issue number6
StatePublished - Nov 2006

Keywords

  • 6 degree of freedom (6DOF) equation
  • CFD
  • Deceleration performance
  • Numerical simulation
  • Rocket ejection seat

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