Finite Element Modeling of Stress Behavior of FGM Nanoplates

Table 4

The maximum values of deflection and stress of FGM nanoplate subjected to uniformly distributed load q₀, n = 1, a/h = 10, a/b = 1, and  = 1.

	Boundary condition
	SSSS	CCCC	CFCF	CFFF
	8.204	2.448	4.934	208.730
	42.885	38.942	71.300	418.320
	42.885	38.942	21.120	125.500
	42.906	6.131	24.540	115.070
	5.743	7.0311	9.629	64.537
	5.743	7.0311	2.802	11.585