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Effect of obliquity on ricochet and cratering for hypervelocity impacts

机译:倾斜对超易撞击术患者的影响

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Numerical simulations were used to investigate ricochet of a mild steel spherical projectile from an aluminum target as a function of impact obliquity for impact velocities of 3.0, 4.0, and 5.0 km/s. Impact obliquity was varied between 50° and 80° in nominally 5° increments, as measured from the normal to the target surface. The impact phenomenology is described and quantified. At these impact velocities, the projectile is highly fragmented from the impact. The mass and momentum of the ricocheted projectile debris, along with the ejection (ricochet) angle, were determined as a function of impact obliquity and velocity. Impact crater dimensions (diameters and depth of penetration) were also determined. It was found that ricochet of the projectile and cratering phenomenology changed dramatically at impact angles of ~70°, at which point the incoming projectile no longer effectively penetrates the target surface. It was also found that many results were independent of impact velocity for the range of velocities considered.
机译:数值模拟用于研究来自铝靶的温和钢球形射弹的Ricochet作为冲击速度的抗冲击速度为3.0,4.0和5.0 km / s的函数。从正常到目标表面测量,撞击倾斜度以标称为5°的增量在50°和80°之间变化。描述和量化影响现象学。在这些冲击速度下,射弹高度碎片从撞击中脱落。作为冲击倾斜和速度的函数确定射精射弹碎片的质量和动量以及喷射(Ricochet)角度。还确定了冲击火山口尺寸(直径和渗透深度)。结果发现,射弹和升降机现象学的Ricochet在〜70°的冲击角度发生急剧变化,此时进入的射弹不再有效地渗透到目标表面。还发现许多结果与考虑的速度范围的冲击速度无关。

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