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双孔式拉瓦尔喷管减后坐结构效能分析

咸东鹏 廖振强 李洪强 李佳圣

弹道学报2013,Vol.25Issue(1):99-102,4.
弹道学报2013,Vol.25Issue(1):99-102,4.

双孔式拉瓦尔喷管减后坐结构效能分析

Performance Analysis of Two-hole Recoilless Structure With Laval Nozzles

咸东鹏 1廖振强 1李洪强 1李佳圣1

作者信息

  • 1. 南京理工大学机械工程学院,南京210094
  • 折叠

摘要

Abstract

In order to study recoilless structures with laval nozzles, a new technical structure was designed,which was two-hole recoilless structure with laval nozzles. The dynamic model of launching process was established by one-dimension two-phase-flow theory. Taking 23 mm test gun as research object,numerical simulation was carried out,and the influence of the distance between the two holes on the muzzle velocity of projectile and the efficiency of reducing recoil force were analyzed. The numerical simulation results were compared with the single-hole front-nozzle structure. Compared with the single-hole front nozzle structure,the best efficiency of reducing recoil force reaches 32. 85% , while the muzzle velocity of projectile don't reduce significantly.

关键词

拉瓦尔喷管/减后坐/数值仿真/两相流/初速

Key words

laval nozzle/reducing recoil force/numerical simulation/two-phase flow/muzzle velocity

分类

军事科技

引用本文复制引用

咸东鹏,廖振强,李洪强,李佳圣..双孔式拉瓦尔喷管减后坐结构效能分析[J].弹道学报,2013,25(1):99-102,4.

弹道学报

OA北大核心CSCDCSTPCD

1004-499X

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