TY - JOUR
T1 - Experimental investigation on the double-position impact responses and damage mechanism for Z-pinned composite laminates
AU - Liao, Binbin
AU - Zhang, Zhongwei
AU - Sun, Liping
AU - Zhou, Jianwu
AU - Wang, Panding
AU - Lin, Yuan
AU - Wu, Wenwang
AU - Fang, Daining
N1 - Publisher Copyright:
© 2020 Elsevier Ltd
PY - 2021/3/1
Y1 - 2021/3/1
N2 - Z-pins can enhance the resistance to delamination for composites effectively under impact loads. In this paper, the effect of Z-pinning technique on double-position low velocity impact behaviors for composite laminates were explored. The two impact positions had the same distance from the center of the laminates with the impact distances of 0 mm, 10 mm, 20 mm and 40 mm in between. The two positions were sequentially impacted with 5 J, 10 J and 20 J impact energy, respectively. The mechanical curves and the delamination damage projected area (DDPA) were recorded during the impact tests. Afterwards, scanning electron microscope (SEM) and X-ray micro-computed tomography (μCT) techniques were performed for characterizing the damage statuses and internal defects. Experimental results demonstrated that Z-pinning was unable to delay the delamination initiation at low impact energy, which led the similar damage statuses of double impact positions by comparing to the unpinned laminates. But at high impact energy, Z-pinning could suppress the delamination damage and internal defects, which weakened the damage interference. In addition, at high impact energy, dominated fiber breakage damage mode occurred for the second impact at the impact distance of 0 mm, accompanied by larger overlapped delamination area with the first impact and lower proportion of internal defects. This resulted in similar values of maximum central displacement and peak energy moment between the unpinned and Z-pinned laminates.
AB - Z-pins can enhance the resistance to delamination for composites effectively under impact loads. In this paper, the effect of Z-pinning technique on double-position low velocity impact behaviors for composite laminates were explored. The two impact positions had the same distance from the center of the laminates with the impact distances of 0 mm, 10 mm, 20 mm and 40 mm in between. The two positions were sequentially impacted with 5 J, 10 J and 20 J impact energy, respectively. The mechanical curves and the delamination damage projected area (DDPA) were recorded during the impact tests. Afterwards, scanning electron microscope (SEM) and X-ray micro-computed tomography (μCT) techniques were performed for characterizing the damage statuses and internal defects. Experimental results demonstrated that Z-pinning was unable to delay the delamination initiation at low impact energy, which led the similar damage statuses of double impact positions by comparing to the unpinned laminates. But at high impact energy, Z-pinning could suppress the delamination damage and internal defects, which weakened the damage interference. In addition, at high impact energy, dominated fiber breakage damage mode occurred for the second impact at the impact distance of 0 mm, accompanied by larger overlapped delamination area with the first impact and lower proportion of internal defects. This resulted in similar values of maximum central displacement and peak energy moment between the unpinned and Z-pinned laminates.
KW - Double-position impact
KW - Internal defects
KW - Mechanical responses
KW - Z-pinned composite laminates
UR - http://www.scopus.com/inward/record.url?scp=85098600497&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2020.113463
DO - 10.1016/j.compstruct.2020.113463
M3 - Article
AN - SCOPUS:85098600497
SN - 0263-8223
VL - 259
JO - Composite Structures
JF - Composite Structures
M1 - 113463
ER -