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