Advances in Materials Science and Engineering / 2018 / Article / Fig 6

Research Article

Strength and Failure Mechanism of Composite-Steel Adhesive Bond Single Lap Joints

Figure 6

Peel and shear stress distributions at three different moments of the joint using 7779 adhesive with 30 mm overlap length. (a) t = 6 s; (b) t = 49 s; (c) t = 110 s.
(a)
(b)
(c)