The numerical and experimental investigation on low-velocity impact response of composite panels: Effect of fabric architecture

2019 ◽  
Vol 227 ◽  
pp. 111343 ◽  
Author(s):  
Hairong Miao ◽  
Zhenyu Wu ◽  
Zhiping Ying ◽  
Xudong Hu
2019 ◽  
Vol 225 ◽  
pp. 111190 ◽  
Author(s):  
Vishwas Mahesh ◽  
Sharnappa Joladarashi ◽  
Satyabodh M. Kulkarni

2020 ◽  
Vol 252 ◽  
pp. 112676
Author(s):  
Tian Zhao ◽  
Yongbo Jiang ◽  
Yangxuan Zhu ◽  
Zhishuai Wan ◽  
Dengbao Xiao ◽  
...  

2011 ◽  
Vol 93 (3) ◽  
pp. 1178-1186 ◽  
Author(s):  
Cesim Atas ◽  
Yalın Akgun ◽  
Olgay Dagdelen ◽  
Bulent M. Icten ◽  
Mehmet Sarikanat

2012 ◽  
Vol 157-158 ◽  
pp. 1135-1138 ◽  
Author(s):  
Mustafizur Rahman ◽  
Evgeny V. Morozov ◽  
Krishna Shankar ◽  
Alan Fien

The present work deals with the finite element modelling of low velocity impact response of different types of composite panels for body armour application. The response of these composites panels including bonded, unbonded and partially bonded laminates has been simulated using non-linear finite element package LS-DYNA. 2D shell elements in LS-DYNA have been used to represent both resin bonded glass fabric targets and dry woven glass fabric panels. The hemispherical shaped projectile is being modelled with 3D solid elements. The results of the numerical analysis showed that the value of contact force for the fully bonded composites panels was significantly higher than that observed for the panels consisting of dry woven glass fabric. However, the corresponding displacement was substantially lower. The similar simulation of the partially bonded composite panels has shown a reduction of both the contact force and the displacement. In addition, it has been shown that the partially bonded composite panels are capable of absorbing higher levels of energy than the rigid panels.


2018 ◽  
Vol 17 ◽  
pp. 31-39 ◽  
Author(s):  
T.K. Demircioğlu ◽  
F. Balıkoğlu ◽  
O. İnal ◽  
N. Arslan ◽  
İ. Ay ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document