节点文献
同心发射筒燃气开盖技术
Techniques for the Automatic Cover Opening in Concentric Canister Launcher
【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.
【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.
【关键词】 同心筒发射装置;
计算流体力学;
数值计算;
【Key words】 concentric canister launcher; computational fluid dynamics; numerical calculation;
【Key words】 concentric canister launcher; computational fluid dynamics; numerical calculation;
【基金】 国家自然科学基金资助项目(60171018)
- 【文献出处】 北京理工大学学报 ,Journal of Beijing Institute of Technology , 编辑部邮箱 ,2004年04期
- 【分类号】TJ760
- 【被引频次】34
- 【下载频次】440