研究发射一系列弹头时,某些因素对弹头偏离角的影响

Vo Van Bien, Hoang Duy Vinh, Tran Van Manh, Nguyen Minh Phu
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引用次数: 0

摘要

本文建立了一个方程,用于确定考虑到若干射弹参数影响的射弹偏离角。弹丸参数包括:发射时围绕旋转部件轴线的旋转速度;弹丸温度导致的炮管曲率。数值计算适用于 37 毫米高射炮。研究结果表明发射时围绕旋转部件轴线的旋转速度对所有类型的火炮都有显著影响,尤其是对长管火炮;而在串联发射时,弹丸温度会显著影响弹头的离去角。这种影响会造成发射误差。当旋转速度越快时,偏离角越大;当考虑到弹丸温度时,发射第 5、10 和 15 枚弹丸时的偏离角分别为 0.0117、0.015、0.0175、0.0185、0.0199 和 0.0206 拉德。这一结果可作为提供有效枪管设计方案和枪管冷却方法的数据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
RESEARCH ON THE INFLUENCE OF SOME FACTORS ON THE DEPARTURE ANGLE OF WARHEADS WHEN FIRING A SERIES
In this article, the equation for determining the projectile's departure angle taking into account the effects of several shot parameters is established. The parameters of the shot include the speed of rotation around the axis of the rotating part when fired; and the curvature of the barrel due to the temperature of the shot. Numerical calculations are applied to 37mm anti-aircraft guns. Research results show that: The speed of rotation around the axis of the rotating part when firing has a significant effect on all types of artillery, especially on long-barreled artillery; While the shot temperature significantly affects the departure angle of the warhead when firing in series. This influence causes errors in the firing. The departure angle becomes larger as the rotation speed becomes faster; The departure angle of the bullet when firing the 5th, 10th, and 15th bullets is 0.0117, 0.015, 0.0175, 0.0185, 0.0199, and 0.0206 rad, respectively, when taking into account the shot temperature. This result is used as data to provide effective barrel design solutions and barrel cooling methods
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