Axisymmetric analysis of auxetic composite cylindrical shells with honeycomb core layer and variable thickness subjected to combined axial and non-uniform radial pressures-Reference-Cited by-同舟云学术

Axisymmetric analysis of auxetic composite cylindrical shells with honeycomb core layer and variable thickness subjected to combined axial and non-uniform radial pressures

Published:2020-10-30 Issue: Volume: Page:1-15
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

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. Faculty of Science, Technology and Environment, School of Engineering and Physics, The University of the South Pacific (USP), Suva, Fiji

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15376494.2020.1841346

Reference42 articles.

1. Axisymmetric Vibrations of a Vessel with Variable Thickness

2. Closed form solution for displacements of thick cylinders with varying thickness subjected to non-uniform internal pressure

3. Bending Analysis of Symmetrically Laminated Cylindrical Panels Using the Extended Kantorovich Method

4. Vibration and stability of composite cylindrical shells containing a FG layer subjected to various loads

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