TY  - JOUR
Y1  - 2014///
UR  - https://www.scopus.com/inward/record.uri?eid=2-s2.0-84920705165&doi=10.1007%2fs12206-014-0801-3&partnerID=40&md5=3b08219cc8e2d410b0391a396d5c0648
A1  - Albarody, T.M.B.
A1  - Al-Kayiem, H.H.
JF  - Journal of Mechanical Science and Technology
VL  - 28
N2  - Modeling of piezo-laminated shell structure and/or shell embedded smart lamina influenced by thermo-magneto-electro-elastic load presents a challenge to be formulated and solved. We derived an analytical model based on the first-order transversally shear deformation theory with involvement of Codazzi-Gauss geometrical discretion. The present invented model and the desired boundary conditions were rigorouslyderived using Hamiltonâ??s principle with cooperationof Gibbs free energy functions. The model was castin theversion of a general laminated composite shell of revolution, in order to be simplified to account for most occurring shell geometries, and intended for wide range of smart materials. To ensure a conventional effective medium model, a rectangular plane shell of zero and large curvatures wasselected for analysis to justify the model. Hence, the generic forced-solution procedures for the response were derived, and its natural frequencies were evaluated in a simply supported boundary condition. Investigatedexamples areaccompanied and noteworthy conclusions drawn which highlight the issues of the implementation of the exact solution, implication of the effects of the material properties, lay-ups of the constituent layers, and shell parameters on the free vibrational behavior. © 2014, The Korean Society of Mechanical Engineers and Springer-Verlag Berlin Heidelberg.
IS  - 12
KW  - Boundary conditions; Free energy; Gibbs free energy; Laminating; Shear deformation; Shells (structures)
KW  -  Laminated shell; Linear analysis; Magneto electro elastic; Smart composites; Structronic shell
KW  -  Laminated composites
ID  - scholars4092
SN  - 1738494X
PB  - Korean Society of Mechanical Engineers
EP  - 4891
AV  - none
N1  - cited By 16
TI  - Dynamic analysis of laminated composite thermo-magneto-electro-elastic shells
SP  - 4877
ER  -