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壳体形状对云爆战斗部抛撒云团尺寸的影响 被引量:1
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作者 许志峰 尹俊婷 +1 位作者 何超 刘扬 《中北大学学报(自然科学版)》 CAS 2018年第6期672-676,701,共6页
通过对某云爆战斗部进行三组相同装药量不同壳体形状的爆炸抛撒实验,研究了壳体形状对云爆战斗部抛撒云团尺寸的影响.结果表明,在50ms时,该云爆战斗部采用圆锥形壳体时抛撒云团直径最大,比圆柱形壳体抛撒云团直径大8%,比柱锥形壳体抛撒... 通过对某云爆战斗部进行三组相同装药量不同壳体形状的爆炸抛撒实验,研究了壳体形状对云爆战斗部抛撒云团尺寸的影响.结果表明,在50ms时,该云爆战斗部采用圆锥形壳体时抛撒云团直径最大,比圆柱形壳体抛撒云团直径大8%,比柱锥形壳体抛撒云团直径大41%;而且采用圆锥形壳体时抛撒云团高度最小.由此可知,采用圆锥形壳体可以增大抛撒云团的面积及能量密度,进而增大云团起爆后的毁伤效果,这一结论可为云爆战斗部壳体结构设计提供参考. 展开更多
关键词 云爆战斗部 壳体形状 爆炸抛撒 云团直径 云团高度
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轴向和环向双聚焦破片战斗部壳体形状设计 被引量:2
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作者 李翔宇 张绍兴 +1 位作者 李振铎 梁民族 《装甲兵工程学院学报》 2018年第2期64-68,共5页
破片定向聚焦是战斗部实现高效毁伤的重要途径。基于Shapiro公式和壳体微元分析方法,提出一种轴向和环向双聚焦破片战斗部壳体形状设计方法,可根据需要的聚焦程度设计对应的壳体形状,利用LS-DYNA中ALE算法对设计的壳体飞散过程进行数值... 破片定向聚焦是战斗部实现高效毁伤的重要途径。基于Shapiro公式和壳体微元分析方法,提出一种轴向和环向双聚焦破片战斗部壳体形状设计方法,可根据需要的聚焦程度设计对应的壳体形状,利用LS-DYNA中ALE算法对设计的壳体飞散过程进行数值模拟,并考察了壳体形状对破片分布的影响。结果表明:设计的壳体可实现破片在轴向和环向2个方向聚焦飞散,从而获得较大的破片密度增益。 展开更多
关键词 破片战斗部 轴向和环向双聚焦 壳体形状 Shapiro公式
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AZ31镁合金复杂形状壳体拉深成形试验研究
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作者 王忠堂 胡乃铮 +2 位作者 梁海成 张士宏 阮立群 《特种铸造及有色合金》 CAS CSCD 北大核心 2010年第11期1053-1055,共3页
通过拉深成形试验研究了AZ31镁合金复杂形状壳体的成形性能,分析了成形温度、拉深速度、坯料加热时间及润滑等工艺参数对镁合金手枪壳体拉深成形件质量的影响规律。结果表明,合理的成形工艺参数:成形温度为290~350℃,拉深速度为0.1~0.... 通过拉深成形试验研究了AZ31镁合金复杂形状壳体的成形性能,分析了成形温度、拉深速度、坯料加热时间及润滑等工艺参数对镁合金手枪壳体拉深成形件质量的影响规律。结果表明,合理的成形工艺参数:成形温度为290~350℃,拉深速度为0.1~0.2mm/s,加热时间为5~10min,润滑剂采用二硫化钼和机油的混合物,成功地加工出合格的复杂形状的镁合金手枪壳体。 展开更多
关键词 AZ31镁合金 复杂形状 拉深
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复杂形状壳体数控加工研究 被引量:1
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作者 陈建宁 何超 袁江 《火箭推进》 CAS 2010年第4期49-52,58,共5页
应用UG CAM对复杂形状壳体进行机床仿真加工,避免了实际加工中存在的问题,提高了产品加工效率和质量,解决了以往壳体加工变形的问题。同时,为保证产品批次质量的稳定性,提出了采用可视化工艺文件的建议。
关键词 复杂形状 虚拟制造 可视化数控工艺
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任意形状薄壳统一的非线性稳定性方程
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作者 李忱 黄执中 《电力学报》 1993年第3期7-11,共5页
关键词 任意形状 非线性 稳定性方程
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Formation mechanism and criterion of linear segregation in ZL205A alloy 被引量:9
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作者 王晔 吴士平 +3 位作者 薛祥 陈瑞润 张建兵 肖文峰 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第11期3632-3638,共7页
The experiments and numerical simulation were conducted for ZL205A aluminum alloy cylindrical shell casting. The formation mechanism of the linear segregation produced by the low pressure die casting (LPDC) process wa... The experiments and numerical simulation were conducted for ZL205A aluminum alloy cylindrical shell casting. The formation mechanism of the linear segregation produced by the low pressure die casting (LPDC) process was investigated. And the heat transfer of the casting during solidification process was analyzed by simulation technique, resulting from the information of linear segregation obtained by plenty of experiments. The new linear segregation criterion was proposed through the simulation and experimental results. It was found that the melting metal with high Cu contents was feeding the crack shrinkage formed by the tearing under the effect of feeding pressure during the later solidification, which led to the formation of linear segregation. The control methods for the linear segregation were suggested based on the proposed mechanism. Finally, the criterion of linear segregation was confirmed by the production of the actual castings. 展开更多
关键词 cylindrical shell casting linear segregation formation mechanism CRITERION control method
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Generatrix shape optimization of stiffened shells for low imperfection sensitivity 被引量:6
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作者 WANG Bo HAO Peng +3 位作者 LI Gang WANG XiaoJun TANG XiaoHan LUAN Yu 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第10期2012-2019,共8页
According to previous studies,stiffened shells with convex hyperbolic generatrix shape are less sensitive to imperfections.In this study,the effects of generatrix shape on the performances of elastic and plastic buckl... According to previous studies,stiffened shells with convex hyperbolic generatrix shape are less sensitive to imperfections.In this study,the effects of generatrix shape on the performances of elastic and plastic buckling in stiffened shells are investigated.Then,a more general description of generatrix shape is proposed,which can simply be expressed as a convex B-spline curve(controlled by four key points).An optimization framework of stiffened shells with a convex B-spline generatrix is established,with optimization objective being measured in terms of nominal collapse load,which can be expressed as a weighted sum of geometrically imperfect shells.The effectiveness of the proposed framework is demonstrated by a detailed comparison of the optimum designs for the B-spline and hyperbolic generatrix shapes.The decrease of imperfection sensitivity allows for a significant weight saving,which is particularly important in the development of future heavy-lift launch vehicles. 展开更多
关键词 stiffened shell COLLAPSE imperfection sensitivity generatrix shape optimization
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