Research Article

Nonlinear Vibrations of 3D Laminated Composite Beams

Table 7

Static deformations of the transverse displacement , layers [90°/0°].

Force
(106 N)
57101213141517

Current model−0.1339−0.1641−0.1993−0.2187−0.2275−0.2358−0.2436−0.2583
Reference [31] −0.1341−0.1645−0.1999−0.2193−0.2281−0.2365−0.2444−0.2591
Difference %0.170.230.290.280.280.280.310.30