Vibration analysis of graphene oxide powder-/carbon fiber-reinforced multi-scale porous nanocomposite beams: A finite-element study

被引:53
作者
Ebrahimi, Farzad [1 ]
Dabbagh, Ali [2 ]
机构
[1] Imam Khomeini Int Univ, Fac Engn, Dept Mech Engn, Qazvin, Iran
[2] Univ Tehran, Coll Engn, Sch Mech Engn, Tehran, Iran
关键词
SHEAR DEFORMATION-THEORY; LAMINATED COMPOSITE PLATES; THERMAL BUCKLING ANALYSIS; VELOCITY IMPACT RESPONSE; FUNCTIONALLY GRADED PLATES; NONLINEAR FREE-VIBRATION; ISOGEOMETRIC ANALYSIS; POSTBUCKLING ANALYSIS; SANDWICH PLATES; ELASTIC FOUNDATIONS;
D O I
10.1140/epjp/i2019-12594-1
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
.Application of the Rayleigh-Ritz method for the vibration problem of a porous multi-scale hybrid nanocomposite graphene oxide powder (GOP)/carbon fiber (CF)-reinforced beam is shown here for the first time on the basis of a new refined higher-order shear deformation beam theory. The structure consists of an initial matrix which is strengthened via both macro- and nano-scale reinforcements. Herein, GOPs and CFs are selected to be dispersed inside the resin. Moreover, the influences of porosity are included, too. The governing equations of the problem are achieved in the framework of a new refined higher-order beam model. Afterward, the Rayleigh-Ritz well-known finite-element method (FEM) is implemented to solve the problem for various boundary conditions (BCs). The validity of the presented formulation is checked by comparing the results of the employed FEM with those achieved from the Navier solution. it is shown that hybrid nanocomposites are able to support higher natural frequencies in comparison with either conventional fiber-reinforced composites or common two-phase GOP-reinforced nanocomposites.
引用
收藏
页数:15
相关论文
共 105 条
[1]   An efficient hyperbolic shear deformation theory for bending, buckling and free vibration of FGM sandwich plates with various boundary conditions [J].
Abdelaziz, Hadj Henni ;
Meziane, Mohamed Ait Amar ;
Bousahla, Abdelmoumen Anis ;
Tounsi, Abdelouahed ;
Mahmoud, S. R. ;
Alwabli, Afaf S. .
STEEL AND COMPOSITE STRUCTURES, 2017, 25 (06) :693-704
[2]   A novel quasi-3D trigonometric plate theory for free vibration analysis of advanced composite plates [J].
Abualnour, Moussa ;
Houari, Mohammed Sid Ahmed ;
Tounsi, Abdelouahed ;
Bedia, El Abbes Adda ;
Mahmoud, S. R. .
COMPOSITE STRUCTURES, 2018, 184 :688-697
[3]   Free vibration and buckling analysis of cross-ply laminated composite plates using Carrera's unified formulation based on Isogeometric approach [J].
Alesadi, Amirhadi ;
Galehdari, Marzieh ;
Shojaee, Saeed .
COMPUTERS & STRUCTURES, 2017, 183 :38-47
[4]   Buckling and vibration analysis of embedded functionally graded carbon nanotube-reinforced composite annular sector plates under thermal loading [J].
Ansari, Reza ;
Torabi, Jalal ;
Shojaei, Mostafa Faghih .
COMPOSITES PART B-ENGINEERING, 2017, 109 :197-213
[5]   Vibration behavior of visco-elastically coupled sandwich beams with magnetorheological core and three-phase carbon nanotubes/fiber/polymer composite facesheets subjected to external magnetic field [J].
Arani, A. Ghorbanpour ;
Zarei, H. BabaAkbar ;
Eskandari, M. ;
Pourmousa, P. .
JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2019, 21 (07) :2194-2218
[6]   Vibration characteristics of a fiber-reinforced polymer bridge superstructure [J].
Aref, AJ ;
Alampalli, S .
COMPOSITE STRUCTURES, 2001, 52 (3-4) :467-474
[8]   A new shear deformation theory for laminated composite plates [J].
Aydogdu, Metin .
COMPOSITE STRUCTURES, 2009, 89 (01) :94-101
[9]   Dynamic and bending analysis of carbon nanotube-reinforced composite plates with elastic foundation [J].
Bakhadda, Boumediene ;
Bouiadjra, Mohamed Bachir ;
Bourada, Fouad ;
Bousahla, Abdelmoumen Anis ;
Tounsi, Abdelouahed ;
Mahmoud, S. R. .
WIND AND STRUCTURES, 2018, 27 (05) :311-324
[10]   Vibration analysis of functionally graded graphene platelet reinforced cylindrical shells with different porosity distributions [J].
Barati, Mohammad Reza ;
Zenkour, Ashraf M. .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2019, 26 (18) :1580-1588