Finite Element Modeling of Laminated Composite Plates with Locally Delaminated Interface Subjected to Impact Loading

Figure 4

Displacement history of laminate with 𝐴_𝑟=0.88 for (a) [0/0], (b) [30/0], (c) [50/0], and (d) [90/0] laminates.

(a)

(b)

(c)

(d)