Largest Lyapunov Exponent Parameter of Stiffened Carbon Fiber Reinforced Epoxy Composite Laminated Plate Due to Critical Buckling Load Using Average Logarithmic Divergence Approach

The purpose of this study is to calculate the bending deflection which used investigate largest Lyapunov exponent due buckling load. design methodology parameter at different thickness ratios and fiber volume fractions using one two stiffeners in order reduce chaotic phenomenon. practical implication find a strain gauge through meter, algorithm average logarithmic divergence experimentally. experiment set up carried out Southwell plot when upper head servo hydraulic cylinder moves downward. There are no limitations research, since it works on all kinds composite materials, ratios, number layers, fractions, boundary conditions. findings work will allow us detect phenomenon stiffened carbon reinforced epoxy laminated plate conception parameter. higher shear deformation theory (HOSDT) plates analytically data against time. All systems paper have non-periodic motion chaos because value above zero. originality use code presence based plate.