D型战斗部与战机目标的最优交会角研究
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山西省基础研究计划资助项目(202303021212190)


Research on the optimum intercept angle between D-shaped warhead and aircraft object
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    摘要:

    为了解决传统战斗部在应对高机动、高空、高速战机目标时存在的制导精度不足与毁伤效能有限等问题,采用具有定向毁伤特性的D型战斗部,通过系统优化毁伤参数和能量传递路径,构建了针对高速战机目标的高效毁伤体系;基于Autodyn仿真平台建立120° D型战斗部侵彻战机复合蒙皮模型,结合7种常见工况,选取破片威力最大的情况对战斗部座舱壳体的最优交会角进行评估。结果表明:动态爆炸中破片飞散速度增强,且方向倾斜;当破片相对速度垂直战机速度时(交会角为45.96°),座舱壳的侵穿效果最佳;推导的破片初速公式与交会角公式具有适用性。研究可为快速计算D型战斗部与战机目标最优交会角提供理论基础。

    Abstract:

    To address the problem of insufficient guidance accuracy and limited damage effectiveness of traditional warheads when engaging highly maneuverable, high-altitude, and high-speed fighter aircraft, a D-shaped warhead with directional damage characteristics was adopted. By systematically optimizing damage parameter and energy transfer path, an efficient damage system tailored for high-speed fighter targets was constructed. A penetration model of a 120° D-shaped warhead against the composite skin of fighter aircraft was developed based on the Autodyn simulation platform. Considering seven common conditions, the case yielding the highest fragment lethality was selected to evaluate the optimal interception angle for damaging the cockpit canopy. The results indicate that during dynamic detonation, fragment dispersion velocity increases with a directional tilt. The penetration effect on the cockpit canopy is maximized when the relative fragment velocity is perpendicular to the aircraft's velocity (interception angle of 45.96°). The derived formulas for initial fragment velocity and interception angle demonstrate universal applicability. This research provides a theoretical basis for rapidly calculating the optimal interception angle between D-shaped warheads and fighter targets.

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张壮壮,张冬梅,张 宇,杜东艳. D型战斗部与战机目标的最优交会角研究[J].河北工业科技,2025,42(5):469-478

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  • 收稿日期:2025-04-02
  • 最后修改日期:2025-07-12
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  • 在线发布日期: 2025-10-09
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