Failure load prediction of composite bolted joint with clamping force

2018 ◽  
Vol 189 ◽  
pp. 247-255 ◽  
Author(s):  
Jae-Il Choi ◽  
Seyyed Mohammad Hasheminia ◽  
Heoung-Jae Chun ◽  
Jong-Chan Park ◽  
Hong Suk Chang
2016 ◽  
Vol 26 (2) ◽  
pp. 115-133 ◽  
Author(s):  
Viet-Hoai Truong ◽  
Jae-Seung Yoo ◽  
Choong-Hyun Kim ◽  
Min-Young Park ◽  
Jin-Ho Choi ◽  
...  

2020 ◽  
Vol 108 ◽  
pp. 102531
Author(s):  
Jérémy Le Pavic ◽  
Thomas Bonnemains ◽  
Éric Lolive ◽  
Georgios Stamoulis ◽  
David Da Silva ◽  
...  

2008 ◽  
Vol 20 (3) ◽  
pp. 445-453 ◽  
Author(s):  
S. L. Manske ◽  
T. Liu-Ambrose ◽  
D. M. L. Cooper ◽  
S. Kontulainen ◽  
P. Guy ◽  
...  

2011 ◽  
Vol 250-253 ◽  
pp. 742-745
Author(s):  
Zhen Qing Wang ◽  
Song Zhou ◽  
Ji Feng Zhang ◽  
Xiao Qiang Wang

Composite materials have excellent mechanical properties and can be mechanically tailor designed, so the composite materials are widely used in civil engineering and structural system such as aerospace and shipbuilding industry. Numerous studies show that the damage of joints is main reason which results in composite structure failure. In this paper, extended finite element method (XFEM) is applied to investigate the failure load prediction of bolted single-lap composite joint. The influences of geometric parameter: edge-to-diameter (E/D) on failure load is investigated.


Sign in / Sign up

Export Citation Format

Share Document