Analysis of ejection after-effect for underwaterlaunched emulating missile

Han Ping Wang*, You Sheng Wu, Dong Cheng, Wen Hui Yu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

8 Citations (Scopus)

Abstract

2D axi-symmetric simulation models for underwater-launched emulating missile ejection aftereffect were built up based on mixture multi-phase model and dynamic meshing technology, which took the cavitations and vaporization effect into consideration. Through simulation, time-variable velocity characteristics of underwater missile, effect of balance gas and vaporization on ejection after-effect were achieved. Simulation results showed that effect of balance gas on after-effect was remarkable, and that of vaporization was negligible. This research method and its conclusions are a good kind of reference to analysis of pressure field near canister outlet and design of the water ballistics of underwater-launched missile.

Original languageEnglish
Pages (from-to)1122-1128
Number of pages7
JournalChuan Bo Li Xue/Journal of Ship Mechanics
Volume14
Issue number10
Publication statusPublished - Oct 2010

Keywords

  • After-effect
  • Cavitations
  • Ejection
  • Multiple phase flow
  • Underwater launcher
  • Underwater missile
  • Vaporization

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