Peridynamic Open-Hole Tensile Strength Prediction of Fiber-Reinforced Composite Laminate Using Energy-Based Failure Criteria

Table 1

Specimen configuration of composite laminates with open-hole.

Specimen	Material system	L	W	D	Thickness	Layup	h (ply)
OHT1 [25]	IM7/8552	64	16	3.175	1	[90/45/0/-45]S	0.125
OHT2 [17]	IM-7/977-3	138.43	38.1	6.35	2	[0/45/90/-45]2S	0.125
OHT3 [34]	IM7/8552	100	36	6	3.144	[90/0/45/-45]3S	0.131

Unit: mm.