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潜射导弹筒盖系统附加气室降载技术

王汉平 吴友生

弹道学报2011,Vol.23Issue(1):102-106,5.
弹道学报2011,Vol.23Issue(1):102-106,5.

潜射导弹筒盖系统附加气室降载技术

Add-on Gas Chamber Technique for Depressing Load Over Cover System of Underwater-launched Missile

王汉平 1吴友生2

作者信息

  • 1. 北京理工大学宇航学院,北京,100081
  • 2. 郑州机电工程研究所,郑州,450015
  • 折叠

摘要

Abstract

An add-on gas chamber technique for depressing load over cover system of underwaterlaunched missile was brought forward. Using 2-D axisymmetric model based on dynamic meshing technology and VOF model without phase transformation, the effects of volume and interface length of add-on gas chamber on load characteristics over cover system were modeled and simulated. According to different volume of add-on gas chamber and different interface length, four binds of working conditions were chosen. The results of different working conditions were compared and analyzed. Using this load-depressing technique,load characteristic over the cover is reduced obviously. The peak of negative pressure can depress load only when the volume of addon gas chamber is big enough and the interface is long enough. The bigger the volume of add-on gas chamber and the longer the interface, the more obvious the effect of depressing load over cover system. The result offers reference for depressing load over cover system.

关键词

潜射发射装置/潜射导弹/压力场/VOF模型/多相流/动网格

Key words

underwater launcher/ underwater-launched missile/ pressure field/ VOF model/ multiphase fluid/ dynamic meshing

分类

军事科技

引用本文复制引用

王汉平,吴友生..潜射导弹筒盖系统附加气室降载技术[J].弹道学报,2011,23(1):102-106,5.

弹道学报

OA北大核心CSCDCSTPCD

1004-499X

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