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对空近炸战斗部的最优设计

OPTIMUM DESIGN FOR ANTIAIRCRAFT MISSILE WARHEADS
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摘要 本文以触发式或近炸式小型导弹战斗部为研究对象,建立了以破片杀伤飞机要害舱段中典型舱段的比动能和总体设计对战斗部的9个约束函数,以及以“杀爆相关毁伤效应”为目标函数的工程优化设计数学模型。采用SUMT-DFP法求解。 This paper deals with the optimum design of mini-missile warheads of the proximity or contact type. Nine restraining functions including requirments of specific kinetic energy for fragments damaging the typical fated cabins of an aircraft, and the requirment of overall design for the warhead are established Mathematical model is set up for engineering optimization in which the interrelated fragmentation-blasting damage effect has been taken as the target function The solution is worked out by using SUMT-DFP method.
出处 《兵工学报》 EI CAS CSCD 北大核心 1989年第3期11-16,共6页 Acta Armamentarii
关键词 战斗部 弹药 最优设计 终点效应 warhead, ammunition, optimum design, terminal effect
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参考文献1

  • 1冯顺山,蒋浩征.爆炸冲击波与杀伤破片对飞机目标相关毁伤效应的研究[J]北京工业学院学报,1986(01).

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