Bending analysis of a micro sandwich skew plate using extended Kantorovich method based on Eshelby-Mori-Tanaka approach

被引:46
作者
Rajabi, Javad [1 ]
Mohammadimehr, Mehdi [1 ]
机构
[1] Univ Kashan, Fac Mech Engn, Dept Solid Mech, POB 87317-53153, Kashan, Iran
关键词
bending analysis; micro sandwich skew plate; piezoelectric composite face sheets; extended Kantorovich method; Eshelby-Mori-Tanaka approach; THERMAL BUCKLING ANALYSIS; FREE-VIBRATION ANALYSES; CARBON NANOTUBES; STABILITY ANALYSIS; MAGNETIC-FIELD; SECTOR PLATES; FREE-FORM; COMPOSITE; BEHAVIOR; PANELS;
D O I
10.12989/cac.2019.23.5.361
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this research, bending analysis of a micro sandwich skew plate with isotropic core and piezoelectric composite face sheets reinforced by carbon nanotube on the elastic foundations are studied. The classical plate theory (CPT) are used to model micro sandwich skew plate and to apply size dependent effects based on modified strain gradient theory. Eshelby-Mori-Tanaka approach is considered for the effective mechanical properties of the nanocomposite face sheets. The governing equations of equilibrium are derived using minimum principle of total potential energy and then solved by extended Kantorovich method (EKM). The effects of width to thickness ratio and length to width of the sandwich plate, core-to-face sheet thickness ratio, the material length scale parameters, volume fraction of CNT, the angle of skew plate, different boundary conditions and types of cores on the deflection of micro sandwich skew plate are investigated. One of the most important results is the reduction of the deflection by increasing the angle of the micro sandwich skew plate and decreasing the deflection by decreasing the thickness of the structural core. The results of this research can be used in modern construction in the form of reinforced slabs or stiffened plates and also used in construction of bridges, the wing of airplane.
引用
收藏
页码:361 / 376
页数:16
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