Figure 11. The 1st buckling mode of the composite plate with twelve layers and orientation of layers [90 0 90] and loaded by a) compression load, b) shear load, c) combination of compression and shear load

From

The Buckling Analysis of the Composite Plates with Different Orientations of Layers

Pavol Lengvarský, Jozef Bocko, Martin Hagara

American Journal of Mechanical Engineering. 2016, 4(7), 413-417 doi:10.12691/ajme-4-7-33