نویسندگان | مسعود مهندس,احمدرضا قاسمی |
---|---|
نشریه | Mechanics of Advanced Composite Structures |
شماره صفحات | 105 |
شماره مجلد | 6 |
نوع مقاله | Full Paper |
تاریخ انتشار | 2019-11-24 |
رتبه نشریه | علمی - پژوهشی |
نوع نشریه | الکترونیکی |
کشور محل چاپ | ایران |
نمایه نشریه | SCOPUS ,ISC |
چکیده مقاله
In this study, discrepancies between the free vibration of fiber-metal laminate (FML) and com-posite cylindrical shells reinforced by carbon nanotubes (CNTs) based on Love’s first approxi-mation shell theory have been considered by beam modal function model. The representative volume elements consist of three and four phases for composite and FML structures, respec-tively, which include fiber, CNTs, polymer matrix and metal for FML cylindrical shells while the metal section is ignored for composite cylindrical shells. The modulus of carbon nanotubes rein-forced composites cylindrical shell could be defined based on rule of mixture. In addition, the fiber phase can be reinforced by the obtained matrix using the extended rule of mixture. The frequencies of FML and composite cylindrical shells reinforced by CNTs have been compared to each other for different materials, lay-ups, boundary conditions, axial and circumferential wave numbers.
tags: Free vibrationFML and composite cylindrical shellsCNTsBeam modal function model