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Geometrically non-linear analysis of FG-CNTRC shell structures with surface-bonded piezoelectric layers
被引:41
|作者:
Mallek, H.
[2
]
Jrad, H.
[2
]
Algahtani, A.
[1
,3
]
Wali, M.
[1
,2
]
Dammakh, F.
[2
]
机构:
[1] King Khalid Univ, Coll Engn, Dept Mech Engn, Abha, Saudi Arabia
[2] Univ Sfax, Natl Engn Sch Sfax, Lab Electromech Syst LASEM, Route Soukra Km 4, Sfax 3038, Tunisia
[3] King Khalid Univ, Res Ctr Adv Mat Sci, POB 9004, Abha 61413, Asir, Saudi Arabia
关键词:
Functionally graded carbon nanotubes;
Geometrically non-linear analysis;
Piezoelectric layers;
Smart thin structures;
Kirchhoff shell model;
FREE-VIBRATION ANALYSIS;
FINITE-ELEMENT-METHOD;
REINFORCED COMPOSITE PLATES;
FUNCTIONALLY GRADED PLATES;
POSTBUCKLING ANALYSIS;
NUMERICAL-ANALYSIS;
SANDWICH PLATES;
ACTIVE CONTROL;
SENSORS;
BEAMS;
D O I:
10.1016/j.cma.2019.01.001
中图分类号:
T [工业技术];
学科分类号:
08 ;
摘要:
This work makes a first attempt to conduct a geometrically non-linear analysis of functionally graded carbon nanotube reinforced composites (FG-CNTRC) structures, with surface-bonded active layers, based on Kirchhoff shell theory. Uniform and three different distribution types of functionally graded nanocomposites are presented. These distributions are assumed to be uniaxially aligned in the axial direction and functionally graded in the shell thickness direction, while the electric potential through the thickness of the active layers is assumed to be linear. A comparison study is carried out in order to show the applicability of the current formulation applied to various shapes of shell structures. The effects of various parameters as volume fraction, distribution of nanotubes, geometrical characteristics as well as load boundary on non-linear behavior of the smart FG-CNTRC structures are investigated. (C) 2019 Elsevier B.V. All rights reserved.
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页码:679 / 699
页数:21
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