Research Article

Finite Element Modeling of Stress Behavior of FGM Nanoplates

Table 8

Maximum stresses at z = h/2 of fully simply supported FGM nanoplate subjected to uniformly distributed load, a/h = 10, and a/b = 1.

n
00.51.01.52.02.5

048.29849.05649.81450.59351.35052.106
0.557.74058.64559.55060.45661.36162.267
267.76768.82869.89070.95172.01373.074
1085.70387.04288.38189.72091.05992.398

048.29849.05649.81450.50351.35052.126
0.557.74058.58559.55060.45661.36162.267
267.76768.82869.89070.95172.01373.074
1085.70387.04288.38189.72091.05992.398

025.45627.26034.26041.26048.25955.259
0.530.40132.56440.92649.28757.64966.010
235.69638.22848.40357.85967.67577.490
1045.18548.36860.78773.20785.62698.045

03.8933.8943.8953.8963.8973.898
0.54.8524.8534.8544.8554.8564.857
26.4016.4026.4036.4046.4056.406
108.3448.3458.3468.3478.3488.349

03.8933.8943.8953.8963.8973.898
0.54.8524.8534.8544.8554.8564.857
26.4016.4026.4036.4046.4056.406
108.3448.3458.3468.3478.3488.349