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战斗部与发动机协同爆轰毁伤特性

杨珍应, 贾鑫*(), 朱长林, 黄正祥, 郭继康   

  1. (南京理工大学 机械工程学院, 江苏 南京 210094)
  • 收稿日期:2025-03-07 修回日期:2025-06-08
  • 通讯作者: *邮箱:jiaxin@mail.njust.edu.cn
  • 基金资助:
    国家自然科学基金项目(12372360)

Damage Characteristics of Warhead and Engine Synergistic Detonation

YANG Zhenying, JIA Xin*(), ZHU Changlin, HUANG Zhengxiang, GUO Jikang   

  1. (School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China)
  • Received:2025-03-07 Revised:2025-06-08

摘要: 为探究战斗部与发动机协同爆轰的毁伤特性及有效毁伤威力场分布,基于冲击波在刚性壁面的反射,建立了不同强度冲击波相互作用的超压计算模型。利用有限元仿真软件,开展战斗部与不同质量推进剂的发动机协同爆轰的数值模拟计算,获取协同爆轰时不同位置的冲击波参数,分析不同工况下的毁伤增益效果和有效毁伤区域分布特性,结合冲击波对目标的毁伤准则,绘制协同爆轰的有效毁伤区域轮廓线。研究结果表明:战斗部和发动机协同爆轰相比战斗部单独爆轰具有显著的毁伤增益,增益效果与起爆方式、剩余推进剂质量和空间位置相关,当比例距离 <1.25时同步起爆增益较大, >1.75时冲击起爆增益较大,增益效果随剩余推进剂质量和距离的增加而增大;协同爆轰的有效毁伤区域由战斗部轴线毁伤区、发动机轴线毁伤区和径向扇形马赫波毁伤区3部分构成,径向扇形马赫波毁伤区冲击波冲量的增益大于超压的增益;研究结果可为战斗部和发动机协同爆轰及毁伤-推进一体化设计提供参考。

关键词: 协同爆轰, 冲击波, 相互作用, 毁伤推进

Abstract: To investigate the characteristics of damage and effective damage area from the synergistic detonation of combat sections and engine detonation, a overpressure calculation model based on the interaction of different intensity shock waves was established. Utilizing finite element simulation software, numerical simulations of the synergistic detonation of engines with different mass propellants in combat sections were conducted to obtain shock wave parameters at different positions during the synergistic detonation. The damage enhancement effect and effective damage area characteristics under different working conditions were analyzed, and the effective damage contour lines for synergistic detonation were mapped based on the damage criteria of shock waves to the target. The results indicate that the synergistic detonation of combat sections and engines has a significant damage enhancement compared to the detonation of combat sections alone. The enhancement effect is related to the detonation method, the remaining propellant mass, and the spatial position. When the ratio distance < 1.25, simultaneous detonation has a greater enhancement, and when > 1.75, shock detonation has a larger enhancement, and the enhancement effect increases with the remaining propellant mass and distance. The effective damage area of the synergistic detonation consists of three parts: the combat section axis damage area, the engine axis damage area, and the radial Mach wave damage area. The radial Mach wave damage area has a greater enhancement in shock quantity than the enhancement of overpressure. The findings of this study provide a reference for the design of synergistic detonation of combat sections and engines and damage-propulsion integration.

Key words: synergistic detonation, shock wave, interaction, damage-propulsion

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