Research Article

Finite Element Modeling of Stress Behavior of FGM Nanoplates

Table 7

The deflection of fully simply supported FGM nanoplate, a/h = 10, and a/b = 1.

N
00.523510

05.1536.8048.5668.9339.36410.072
0.55.4967.2589.1369.5269.98610.740
1.05.8397.7129.70610.12010.60711.407
1.56.1828.16510.27610.71311.22812.075
2.06.5258.61910.84611.30711.84912.743
2.56.8689.07311.41611.90012.47013.410
3.07.2109.52711.98612.49413.09114.078