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同心发射筒燃气开盖技术
引用本文:苗佩云,袁曾凤.同心发射筒燃气开盖技术[J].北京理工大学学报,2004,24(4):283-285.
作者姓名:苗佩云  袁曾凤
作者单位:北京理工大学,机电工程学院,北京,100081;北京理工大学,机电工程学院,北京,100081
摘    要:为实现导弹自力发射时同心发射筒前盖自动向一侧开启,讨论了4种燃气开盖方案:易碎盖方案、内外筒偏心盖方案、半导流锥方案和各向异性材料发射筒盖方案,并用数值方法模拟了各种方案的筒内复杂三维流场.计算结果表明4种方案均具有可行性.经试验验证,各向异性材料的发射筒盖方案能按预先期望的方向整体飞出.

关 键 词:同心筒发射装置  计算流体力学  数值计算
文章编号:1001-0645(2004)04-0283-03
收稿时间:2003/8/18 0:00:00
修稿时间:2003年8月18日

Techniques for the Automatic Cover Opening in Concentric Canister Launcher
MIAO Pei-yun and YUAN Zeng-feng.Techniques for the Automatic Cover Opening in Concentric Canister Launcher[J].Journal of Beijing Institute of Technology(Natural Science Edition),2004,24(4):283-285.
Authors:MIAO Pei-yun and YUAN Zeng-feng
Institution:School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China
Abstract:In order to open the cover of a concentric canister launcher (CCL) automatically with the jet during its launching, four schemes are put forward, viz.fracturable cover, eccentrically positioned interior and exterior launching tubes, jet guides of assymmetric construction, and covers made of heterogeneous materials. Modes of flow under each scheme are numerically simulated. Detailed data show that all the four schemes are feasible, yet the last named scheme keeps the opened cover intact and makes it fly along the expected direction.
Keywords:concentric canister launcher  computational fluid dynamics  numerical calculation
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