Advances in Materials Science and Engineering / 2012 / Article / Tab 2

Research Article

Optimum Design of Fibre Orientation in Composite Laminate Plates for Out-Plane Stresses

Table 2

Optimum lamina orientations for material T300/5308 under different loads for constant thickness.

Loading: Optimum lamina orientationsSafety factor
(KPa m) (Figure 2)Akbulut and Sonmez [35]Present workAkbulut and Sonmez [35]Present work

200/200/0 2.142.14
200/0/200 4.844.59
400/200/0 1.641.42