Finite Element Modeling of Stress Behavior of FGM Nanoplates

Table 6

Maximum deflection and stress of FGM nanoplate with a hole (R = a/10) subjected to uniformly distributed load, n = 1, a/h = 10, a/b = 1, and .

	Boundary condition
	SSSS	CCCC	CFCF	CFFF
	8.761	2.223	4.961	211.323
	64.686	36.990	76.070	404.569
	64.686	36.990	22.821	121.371
	44.475	6.147	26.410	119.865
	5.520	6.726	9.490	63.296
	5.520	6.726	4.117	52.180