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Bullet Turning at Trajectory Apex

机译:弹道转向尖顶

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摘要

A numerical study is carried out to investigate a 7.62-mm bullet turning at the trajectory apex, particularly when fired vertically. The bullet model includes an aerodynamic model, which basically covers angles of attack up to 180°. Computational fluid dynamics are used to estimate the aerodynamic properties at the high angles of attack. The role of aerodynamic moment, and particularly Magnus phenomena, in turning at the apex is studied. A positive Magnus moment tilts the total aerodynamic moment vector clockwise and generally drives the bullet turning nose down. The bullet turning was detected through a flat spin-type maneuver. The Magnus-moment oscillatory behavior and/or the Magnus-moment-caused bullet instability may occur during the turning at the trajectory apex. These were found to have a negligible effect on the bullet-turning launch angle, but they may contribute considerably to the bullet falling-phase behavior. Possibilities to affect the bullet descending part of the flight are also shortly considered.
机译:进行了数值研究,以研究在弹道顶点处7.62毫米子弹的转动,尤其是垂直发射时。子弹模型包括空气动力学模型,该模型基本上涵盖了高达180°的迎角。计算流体动力学用于估计大迎角的空气动力学特性。研究了空气动力力矩,尤其是马格努斯现象,在转弯顶点时的作用。正的马格努斯力矩使总空气动力学力矩矢量顺时针倾斜,并通常使子弹朝下旋转。通过扁平旋转式机动检测到子弹转向。在轨迹顶点转弯期间可能会发生马格努斯矩的振荡行为和/或马格努斯矩引起的子弹不稳定性。发现这些对子弹转弯发射角的影响可忽略不计,但它们可能对子弹落相行为有很大影响。不久还将考虑影响飞行中子弹下降部分的可能性。

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