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Analytical and experimental studies on ballistic impact behavior of 2D woven fabric composites

机译:二维机织复合材料弹道冲击行为的分析和实验研究

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摘要

A generalized analytical formulation is presented for the prediction of ballistic impact behavior of 2D woven fabric composite laminates impacted with a rigid cylindrical projectile. The formulation is valid for a wide range of laminate thicknesses. The formulation is based on stress wave propagation and energy balance between the projectile and the composite target. During the ballistic impact event, the energy lost by the projectile is absorbed by the target through various damage and energy absorbing mechanisms such as compression of the target directly below the projectile, compression in the region surrounding the impacted zone, shear plugging, stretching and tensile failure of yarns/layers in the region consisting of primary yarns, tensile deformation of yarns/layers in the region consisting of secondary yarns, conical deformation on the back face of the target, delamination, matrix cracking, and friction between the projectile and the target. The formulation presented considers both shear plugging and tensile failure during conical deformation. Solution procedure for the evaluation of ballistic impact performance is presented. Experimental validation is performed on the ballistic impact behavior of two types of composite specimens: 2D plain weave E-glass/epoxy and 2D 8H satin weave T300 carbon/epoxy. Typical results on ballistic limit velocity and energy absorbed by various mechanisms are presented.
机译:提出了一种通用的分析公式,用于预测受刚性圆柱弹丸撞击的2D机织复合材料层压板的弹道冲击行为。该配方适用于各种厚度的层压板。该公式基于弹丸和复合目标之间的应力波传播和能量平衡。在弹道撞击事件中,弹丸损失的能量会通过各种破坏和能量吸收机制被目标吸收,例如,直接压缩弹丸下方的目标的压缩,撞击区域周围区域的压缩,剪切堵塞,拉伸和拉伸由初级纱线组成的区域中纱线/层的破坏,由次级纱线组成的区域中纱线/层的拉伸变形,靶背面的圆锥形变形,分层,基体开裂以及弹丸与靶之间的摩擦。提出的公式考虑了圆锥形变形期间的剪力堵塞和拉伸破坏。提出了评估弹道冲击性能的解决方法。对两种类型的复合材料样品的弹道冲击性能进行了实验验证:2D平纹E型玻璃/环氧树脂和2D 8H缎纹T300碳/环氧树脂。给出了弹道极限速度和各种机制吸收的能量的典型结果。

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