Nondestructive evaluation of impact area on glass fiber reinforced polymer composite by digital image correlation method: experimental study

M. Pakravan, M. Farahani, Amin Barzegar, M. Mahmoudi
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Abstract

The use of non-destructive tests on composite materials to inspect, identify, and observe defects to locate discontinuities or defects has received considerable attention in recent years. Among the existing methods, the use of a non-contact digital image overlay system for troubleshooting composites has been considered because of its advantages. In this research, using the digital image overlay method, the shape, position, and area of the failure area in six-layer glass/epoxy samples with impact damage with different energies under different loads have been investigated. Five composite specimens with impact energies of 5, 10, 20, 30, and 40 joules were tested. At an energy of 5 joules, the damage to the piece was very small, and at an energy of 40 joules, the amount of damage to the piece was such that the bullet got stuck inside the piece and the impact site remained as a hole in the piece. The areas obtained for the impact area in the strain contours at loads of 40% have values close to the actual area of damage. By comparing the area obtained from the strain contour at 40% load and the actual damage area, for the 10 joules, 20 joules, and 30-joule conditions, the difference in area is about 2.3%, about 2.5%, and 3.1%, respectively.
数字图像相关法无损评价玻璃纤维增强聚合物复合材料冲击面积的实验研究
近年来,利用复合材料的无损检测来检测、识别和观察缺陷,以定位不连续或缺陷,受到了相当大的关注。在现有的方法中,利用非接触式数字图像叠加系统对复合材料进行故障排除的方法由于其优点而被考虑。本研究采用数字图像叠加的方法,研究了不同载荷作用下不同能量冲击损伤的六层玻璃/环氧树脂试样的破坏区域形状、位置和面积。测试了冲击能分别为5、10、20、30和40焦耳的5个复合材料试样。在能量为5焦耳的情况下,碎片的损伤非常小,而在能量为40焦耳的情况下,碎片的损伤量如此之大,以至于子弹卡在了碎片内部,而撞击部位仍然是碎片上的一个洞。在载荷为40%时,应变轮廓中获得的冲击区域的值与实际损伤区域接近。在10焦耳、20焦耳和30焦耳条件下,40%载荷下的应变轮廓面积与实际损伤面积的差异分别约为2.3%、2.5%和3.1%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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