Research Article

Influence of Root Rotation on Delamination Fracture Toughness of Composites

Table 3

Critical load and corresponding displacement for the measured crack length of a DCB specimen made of unidirectional carbon/PEEK composite.

Test results Present analysis
Crack length,
(mm)
(N) (mm) (N)
(10)
(mm)
(8)
% relative error in   
(13),
Load Displacement

51120.5910.95119.4811.450.92−4.55119.48
52119.1411.07117.1811.911.65−7.57117.18
53117.0111.89114.9712.371.74−4.02114.97
54115.0612.72112.8412.841.93−0.94112.84
55112.7913.16110.7913.321.78−1.22110.79
60104.4414.77101.5615.852.76−7.32101.56
6596.5617.9893.7418.602.91−3.4693.74
7089.8020.0087.0521.583.06−7.9087.05
7584.9123.6181.2424.774.32−4.9181.24
8076.9826.7276.1728.181.05−5.4576.17

Lay-up: 026,  mm,  mm,  mm,  GPa, , and  J/m2.