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