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

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 is used to investigate the largest Lyapunov exponent due to buckling load. The design methodology is to calculate the largest Lyapunov exponent parameter at different thickness ratios and different fiber volume fractions using on...

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Bibliographic Details
Main Author: Louay S. Yousuf
Format: Article
Language:English
Published: MDPI AG 2022-06-01
Series:Mathematics
Subjects:
Southwell plot
Lyapunov exponent
bending deflection
critical buckling load
average logarithmic divergence
stiffened plate
Online Access:https://www.mdpi.com/2227-7390/10/12/2020

Internet

https://www.mdpi.com/2227-7390/10/12/2020

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