Journal article

New approach to study nonlinear dynamic response and vibration of sandwich composite cylindrical panels with auxetic honeycomb core layer

Dinh Duc Nguyen, Kim Seung-Eock, Duc Tuan Ngo, Tran Phuong, Dinh Khoa Nguyen

Aerospace Science and Technology | ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER | Published : 2017

DOI: 10.1016/j.ast.2017.08.023

Related Projects (1)

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A Bio-Inspired Lightweight Composite System For Blast And Impact Protection

This project aims to develop a lightweight armour system that protects structural elements from extreme loads. Every day around the world, a..

Grants

Awarded by Vietnam National Foundation for Science and Technology Development (NAFOSTED)

Funding Acknowledgements

This research is funded by Vietnam National Foundation for Science and Technology Development (NAFOSTED) under grant number 107.02-2015.03. The authors are grateful for this support.

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Keywords

Science & Technology
Elastic Foundations
Blast
Sandwich Auxetic Composite Cylindrical Panels
Blast and Damping Loads
Engineering, Aerospace
Engineering
Mechanical
Analytical Approach
Ratios
Reddy'S First Order Shear Deformation Theory
Nonlinear Dynamic Response and Vibration
Technology