Forced Vibration Analysis of Laminated Composite Shells Reinforced with Graphene Nanoplatelets Using Finite Element Method

Table 6

Influence of a/h ratio on the nondimensional deflection, velocity, and stress of the centroid point

a/h	10		25		50		75
Maximum value
Temperature
UD-type	0.0052	0.0182	0.0705	0.1464	0.4652	0.6832	1.1324	1.4665
X-type	0.0046	0.0171	0.0616	0.1383	0.4311	0.6469	1.0903	1.4413
O-type	0.0074	0.0212	0.1068	0.2062	0.6239	0.8364	1.4910	1.6342
V-type	0.0065	0.0180	0.0931	0.1846	0.5753	0.7604	1.4027	1.6145
Temperature
UD-type	0.0072	0.0176	0.0873	0.1655	0.5418	0.6793	1.3206	1.5670
X-type	0.0064	0.0164	0.0768	0.1493	0.5058	0.6837	1.2767	1.5529
O-type	0.0100	0.0237	0.1268	0.2251	0.7014	0.9191	1.6752	1.7314
V-type	0.0086	0.0210	0.1097	0.2009	0.6417	0.8327	0.9758	1.6705