| Authors | Thaier J. Ntayeesh,محمد عارفی |
| Journal | Heliyon |
| Page number | 29436 |
| Volume number | 10 |
| IF | 3.4 |
| Paper Type | Full Paper |
| Published At | 2024-04-30 |
| Journal Grade | Scientific - research |
| Journal Type | Electronic |
| Journal Country | Iran, Islamic Republic Of |
| Journal Index | JCR ,SCOPUS |
| Keywords | Piezoelectric/piezomagnetic layers Initial electromagnetic loads Sandwich graphene origami composite plate Thickness stretched plate Micromechanical model Volume fraction Folding degree Temperature |
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Abstract
This work applies a higher order thickness-stretched model for the electro-elastic analysis of the
composite graphene origami reinforced square plate sandwiched by the piezoelectric/piezo-
magnetic layers subjected to the thermal, electric, magnetic and mechanical loads. The plate is
manufactured of a copper matrix reinforced with graphene origami where the effective material
properties are calculated based on the micromechanical models as a function of volume fraction
and folding degree of graphene origami, material properties of matrix, reinforcement, and local
temperature. The governing equations are derived using the virtual work principle in terms of the
bending, shear and stretching functions, in-plane displacements, electric, and magnetic poten-
tials. The numerical results including various displacement components, maximum electric, and
magnetic potentials are presented with changes of volume fraction, folding degree of reinforce-
ment, electrical, magnetic, and thermal loading. A verification investigation is presented for
approve of the methodology, and the solution procedure. The main novelty of this work is
simultaneous effect of the thickness stretching and the multi-field loading on the electromagnetic
bending results of the sandwich plate. Another novelty of this work is usage of graphene origami
nano-reinforcement as a controllable material in a sandwich structure subjected to multi-field
loadings. The results show an increase in bending, shear, and stretching deflections with an in-
crease in electromagnetic loads, and folding degree as well as a decrease in volume fraction of
reinforcement.