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首页> 外文期刊>Journal of Materials Research and Technology >Simulation of CFRP/aluminum foam sandwich structure under high velocity impact
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Simulation of CFRP/aluminum foam sandwich structure under high velocity impact

机译:高速冲击下CFRP /铝泡沫夹层结构的仿真

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摘要

To profoundly reveal the protective performance of CFRP/aluminum foam sandwich structure, the high-speed impact simulation models of CFRP, aluminum foam and their sandwich structures are built by ABAQUS/Explicit module. The VUMAT user material subroutine is written for CFRP panel, and Hashin damage criterion is introduced. The elastic constitutive model and macro modeling method for the aluminum foam are chosen. The impact process under different working conditions is numerically simulated and the reliability of the model is verified by one-stage light gas gun loading experiment at the corresponding simulation conditions. At the same time, the protective performance of CFRP/ aluminum foam sandwich structure under different steel projectile shapes, impact velocities and impact angles (the angle between the ballistic and the target normal line) are simulated. The results show that the Mises stress nephogram of CFRP panel is peanut-like with obvious directivity. The stress wave propagates fastest in the direction perpendicular to the fiber. In the impact velocity range of 172?450 m/s, with the increase of impact velocities, the loss of kinetic energy will increase, but the increase of kinetic energy loss will decrease with the increase of impact velocities, and the contact force between the projectile and the sandwich structure will also increase. Thus the sandwich structure will have more serious delamination and fiber breakage, which will consume more kinetic energy. When the velocity of the projectile is greater than 300 m/s, the impact capability of the sandwich structure tends to the upper limit of impact capacity. In the impact velocity range of 170~300m/s, the sandwich structure has stronger protective performance than ball-nosed projectile when the flat-nosed projectile impact, and the difference of the residual velocity between the two kinds of projectiles is larger. The shape of the projectile has a great influence on the protective performance of the CFRP/ aluminum foam sandwich structure. When the impact velocity is greater than 300m/s, the residual velocities of the two kinds of projectiles are almost the same, and the shapes of the projectile have a gradual effect on the performances of the CFRP/ aluminum foam sandwich structure. The anti-shock performance of sandwich structure under oblique impact is stronger than that of vertical impact. With the increase of impact angles, the transverse deformation of sandwich structure increases, and the anti-shock performance of sandwich structure also increases.
机译:为了深刻揭示CFRP /铝泡沫夹层结构的保护性能,CFRP,铝泡沫及其夹层结构的高速冲击模拟模型由ABAQUS /明确模块构建。 VUMAT用户材料子程序是为CFRP面板编写的,并介绍了Hashin损坏标准。选择弹性本构模型和铝泡沫的宏观建模方法。在数值模拟不同工作条件下的冲击过程,并且在相应的模拟条件下通过单级光气枪载荷实验验证模型的可靠性。同时,模拟了不同钢射弹形状,冲击速度和冲击角下的CFRP /铝泡沫夹层结构的保护性能(弹道和目标正常线之间的角度)。结果表明,CFRP面板的误判压力盖皮是花生的,具有明显的方向性。应力波在垂直于纤维的方向上最快地传播。在172?450米/秒的冲击速度范围内,随着冲击速度的增加,动能的损失将增加,但随着冲击速度的增加,动能损失的增加将降低,以及接触力之间的接触力射弹和夹层结构也将增加。因此,夹层结构将具有更严重的分层和纤维破损,这将消耗更多的动能。当射弹的速度大于300米/秒时,夹层结构的冲击能力趋向于冲击能力的上限。在170〜300m / s的冲击速度范围内,夹层结构具有比球鼻射弹在扁平的射弹冲击的较强的保护性能,以及两种射弹之间的残余速度差异更大。射弹的形状对CFRP /铝泡沫夹层结构的保护性能产生了很大的影响。当冲击速度大于300m / s时,两种射弹的残余速度几乎相同,并且射弹的形状对CFRP /铝泡沫夹层结构的性能具有逐渐影响。斜撞击下夹层结构的抗冲击性能比垂直撞击力强。随着冲击角的增加,夹层结构的横向变形增加,夹层结构的抗冲击性能也增加。

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