A Study of Failure Strength for Fiber-Reinforced Composite Laminates with Consideration of Interface

Table 2

The failure stresses of the 0/90 composite laminates (Mpa).

23°C, no-debonding interface			23°C, debonding interface			650°C, no-debonding interface			650°C, debonding interface
Points	xx-yy	xx-xy	Points	xx-yy	xx-xy	Points	xx-yy	xx-xy	Points	xx-yy	xx-xy
A	1496.1	1496.1	A1	1157.6	1157.6	A	663.2	663.2	A1	621.2	621.2
B	1565.1	873.6	B1	1173.4	574.3	B	663.3	283.2	B1	619.8	255.6
C	−1605.1	−1605.1	C1	−1605.1	−1605.1	C	−677.7	−677.7	C1	−677.7	−677.7
D	−1544.4	−873.5	D1	−1544.4	−567.4	D	−669.4	−283.2	D1	−669.4	−253.5