A closed-form solution for asymmetric free vibration analysis of composite cylindrical shells with metamaterial honeycomb core layer based on shear deformation theory-Reference-Cited by-同舟云学术

A closed-form solution for asymmetric free vibration analysis of composite cylindrical shells with metamaterial honeycomb core layer based on shear deformation theory

Published:2022-03-17 Issue: Volume: Page:1-19
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

Eipakchi Hamidreza¹^ORCID,Mahboubi Nasrekani Farid²^ORCID

Affiliation:

1. Faculty of Mechanical and Mechatronics Engineering, Shahrood University of Technology, Shahrood, I.R. Iran

2. School of Information Technology, Engineering, Mathematics and Physics, The University of the South Pacific (USP), Suva, Fiji

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2022.2051183

Reference50 articles.

1. Stability and asymmetric vibrations of pressurized compressible hyperelastic cylindrical shells

2. Natural frequencies of cylindrical shells and panels in vacuum and in a fluid

3. Free vibrations of functionally graded material cylindrical shell closed with two spherical caps

4. Free vibration of joined conical–cylindrical–conical shells

5. Free vibration analysis of rotating functionally graded conical shells reinforced by anisogrid lattice structure

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