| dc.contributor.author | The Van Tran | |
| dc.contributor.author | Quoc Hoa Pham | |
| dc.contributor.author | Nhan Thinh Hoang | |
| dc.contributor.other | Faculty of Mechanical Engineering, Industrial University of Ho Chi Minh City, Ho Chi Minh City 700000, Vietnam | |
| dc.contributor.other | Tran Dai Nghia University, Ho Chi Minh City, 700000, Vietnam | |
| dc.contributor.other | Faculty of Engineering and Technology, Nguyen Tat Thanh University, Ho Chi Minh City 700000, Vietnam; Corresponding author | |
| dc.date.accessioned | 2025-10-09T05:29:10Z | |
| dc.date.available | 2025-10-09T05:29:10Z | |
| dc.date.issued | 01-07-2023 | |
| dc.identifier.uri | http://www.sciencedirect.com/science/article/pii/S2095034923000326 | |
| dc.identifier.uri | http://digilib.fisipol.ugm.ac.id/repo/handle/15717717/41074 | |
| dc.description.abstract | In this paper, we propose an finite element approach based on classical plate theory to investigate the dynamic stability of a layered composite plate subject to nonlinear aerodynamic load. This study considers the influence of temperature, nonlinear geometry, and nonlinear aerodynamic load on composite plate structures simultaneously. Specifically, the present work conduct comparison the results of the critical pressure value between the nonlinear aerodynamic load and the linear aerodynamic load, thereby pointing out some necessary cases which must consider the nonlinearity of aerodynamic load for calculating the aerospace structures. We determine the critical pressure value and vibrational amplitude response of the plate by means of calculation. The outcomes of our calculations can be useful in designing and repairing body shells and wings of aircraft equipment. | |
| dc.language.iso | EN | |
| dc.publisher | Elsevier | |
| dc.subject.lcc | Engineering (General). Civil engineering (General) | |
| dc.title | Research on stability of laminated composite plate under nonlinear aerodynamic load | |
| dc.type | Article | |
| dc.description.keywords | Finite element approach | |
| dc.description.keywords | Nonlinear aerodynamic load | |
| dc.description.keywords | Composite plate | |
| dc.description.doi | 10.1016/j.taml.2023.100461 | |
| dc.title.journal | Theoretical and Applied Mechanics Letters | |
| dc.identifier.oai | oai:doaj.org/journal:1b65c6b4465e45ecba61ea686a3aaff3 | |
| dc.journal.info | Volume 13, Issue 4 | |
