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
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.