Journal
MECHANICS BASED DESIGN OF STRUCTURES AND MACHINES
Volume 50, Issue 4, Pages 1371-1399Publisher
TAYLOR & FRANCIS INC
DOI: 10.1080/15397734.2020.1752232
Keywords
Multilayered CNTRC nanoplates; angle-ply; cross-ply; buckling; free vibration; higher-order nonlocal strain gradient theory
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This study focuses on the buckling and free vibration of simply-supported cross-ply/angle-ply single-walled carbon nanotubes reinforced composite CNTRC laminated nanoplates in thermal environment. Nonlocal strain gradient theory and third-order shear deformation plate theory are used to analyze the size-dependent effects. The influence of reinforcement patterns, composite structure, nonlocal parameter, length scale parameter, carbon nanotubes orientation, and geometric parameters on buckling loads and natural frequencies is examined.
In this contribution, we analyze buckling and free vibration of simply-supported cross-ply/angle-ply single-walled carbon nanotubes reinforced composite CNTRC laminated nanoplates in thermal environment. The nonlocal strain gradient theory within the third-order shear deformation plate theory are adopted to capture the size-dependent effects of CNTRC laminated nanoplates. Several types of reinforcement material distributions, a uniform distribution and functionally graded distributions, are inspected. Material properties are temperature-dependent and performed using Touloukian principal. The influence of CNTs reinforcement patterns, composite structure, nonlocal parameter, length scale parameter, carbon nanotubes orientation, and the geometric parameters on buckling loads and natural frequencies is examined.
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