Finite Element Modeling of Stress Behavior of FGM Nanoplates

Table 5

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

	Boundary condition
	SSSS	CCCC	CFCF	CFFF
	6.144	2.402	3.912	95.890
	36.239	33.932	51.379	216.270
	36.239	33.844	16.741	64.882
	19.506	6.112	9.305	51.342
	1.964	3.160	4.433	31.929
	0.745	1.715	4.652	6.429