A novel higher-order shear deformation theory for bending and free vibration analysis of isotropic and multilayered plates and shells

被引:134
作者
Zine, Abdallah [1 ,2 ]
Tounsi, Abdelouahed [1 ,3 ]
Draiche, Kada [1 ,4 ]
Sekkal, Mohamed [1 ,3 ]
Mahmoud, S. R. [5 ]
机构
[1] Univ SidiBel Abbes, Fac Technol, Civil Engn Dept, Mat & Hydrol Lab, Sidi Bel Abbes, Algeria
[2] Ctr Univ Relizane, Relizane, Algeria
[3] Univ Djillali Liabes Sidi Bel Abbes, Fac Sci Exactes, Lab Modelisat & Simulat Multiechelle, Dept Phys, Sidi Bel Abbes, Algeria
[4] Univ Ibn Khaldoun, BP 78 Zaaroura, Tiaret 14000, Algeria
[5] King Abdulaziz Univ, Dept Math, Fac Sci, Jeddah, Saudi Arabia
关键词
layered structures; bending; vibration; higher order shear deformation theory; GRADED SANDWICH PLATES; NEUTRAL SURFACE POSITION; LAMINATED COMPOSITE PLATES; THERMAL BUCKLING ANALYSIS; REFINED THEORY; FGM PLATES; POSTBUCKLING BEHAVIOR; MECHANICAL-BEHAVIOR; RECTANGULAR-PLATES; STATIC ANALYSIS;
D O I
10.12989/scs.2018.26.2.125
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
In this work, the bending and free vibration analysis of multilayered plates and shells is presented by utilizing a new higher order shear deformation theory (HSDT). The proposed involves only four unknowns, which is even less than the first shear deformation theory (FSDT) and without requiring the shear correction coefficient. Unlike the conventional HSDTs, the present one presents a novel displacement field which incorporates undetermined integral variables. The equations of motion are derived by using the Hamilton's principle. These equations are then solved via Navier-type, closed form solutions. Bending and vibration results are found for cylindrical and spherical shells and plates for simply supported boundary conditions. Bending and vibration problems are treated as individual cases. Panels are subjected to sinusoidal, distributed and point loads. Results are presented for thick to thin as well as shallow and deep shells. The computed results are compared with the exact 3D elasticity theory and with several other conventional HSDTs. The proposed HSDT is found to be precise compared to other several existing ones for investigating the static and dynamic response of isotropic and multilayered composite shell and plate structures.
引用
收藏
页码:125 / 137
页数:13
相关论文
共 150 条
[1]  
Abdelbari S, 2016, WIND STRUCT, V22, P329
[2]   Thermal buckling response of functionally graded sandwich plates with clamped boundary conditions [J].
Abdelhak, Zohra ;
Hadji, Lazreg ;
Daouadji, T. Hassaine ;
Bedia, E. A. Adda .
SMART STRUCTURES AND SYSTEMS, 2016, 18 (02) :267-291
[3]   Size-dependent mechanical behavior of functionally graded trigonometric shear deformable nanobeams including neutral surface position concept [J].
Ahouel, Mama ;
Houari, Mohammed Sid Ahmed ;
Bedia, E. A. Adda ;
Tounsi, Abdelouahed .
STEEL AND COMPOSITE STRUCTURES, 2016, 20 (05) :963-981
[4]   Mechanical behavior of functionally graded sandwich plates on elastic foundation [J].
Akavci, S. S. .
COMPOSITES PART B-ENGINEERING, 2016, 96 :136-152
[5]   A first-order shear deformation finite element model for elastostatic analysis of laminated composite plates and the equivalent functionally graded plates [J].
Alieldin, S. S. ;
Alshorbagy, A. E. ;
Shaat, M. .
AIN SHAMS ENGINEERING JOURNAL, 2011, 2 (01) :53-62
[6]  
Allen H. G., 2013, ANAL DESIGN STRUCTUR
[7]  
AMBARTSUMIAN S., 1958, IZV OTD TECH NAUK SS, V5, P69
[8]  
[Anonymous], 2014, INT J CIV STRUCT ENV
[9]  
[Anonymous], 1986, 3955 NASA
[10]   A zigzag model for laminated composite beams [J].
Arya, H ;
Shimpi, RP ;
Naik, NK .
COMPOSITE STRUCTURES, 2002, 56 (01) :21-24