eprintid: 2823
rev_number: 8
eprint_status: archive
userid: 354
dir: disk0/00/00/28/23
datestamp: 2017-12-20 04:55:12
lastmod: 2017-12-20 04:55:12
status_changed: 2017-12-20 04:55:12
type: article
metadata_visibility: show
creators_name: Nguyen, Dinh Duc
creators_name: Lee, Jaehong
creators_name: Nguyen, Thoi Trung
creators_name: Pham, Toan Thang
creators_id: ducnd@vnu.edu.vn
title: Static response and free vibration of functionally graded carbon nanotube-reinforced composite rectangular plates resting on Winkler–Pasternak elastic foundations
ispublished: pub
subjects: Mechanics
subjects: isi
divisions: fac_fema
abstract: In the present article, static response and free vibration of functionally graded carbon nanotube
reinforced composite (FG-CNTRC) rectangular plate resting on Winkler–Pasternak elastic foundations
using an analytical approach are studied. The rectangular plates are reinforced by single-walled carbon
nanotubes (SWCNTs) which are assumed to be graded through the thickness direction with four types
of distributions. The mathematical model of the FG-CNTRC plate is developed based on the first-order
shear deformation plate theory (FSDT) and Hamilton principle. By using Navier solution, the governing
equations are solved to obtain the central deflection and the natural frequency parameters. Several
examples are verified to have higher accuracy than those from the previous method in the literature.
Also, the effects of different parameters on static response and natural frequency of FG-CNTRC plate are
highlighted by solving numerous examples. Finally, these new results may serve as benchmarks for future
investigations.
date: 2017
date_type: published
publisher: Elsevier
full_text_status: public
publication: Aerospace Science and Technology
volume: 68
pagerange: 391-402
refereed: TRUE
issn: 1270-9638
citation:   Nguyen, Dinh Duc and Lee, Jaehong and Nguyen, Thoi Trung and Pham, Toan Thang  (2017) Static response and free vibration of functionally graded carbon nanotube-reinforced composite rectangular plates resting on Winkler–Pasternak elastic foundations.  Aerospace Science and Technology, 68 .   pp. 391-402.  ISSN 1270-9638     
document_url: https://eprints.uet.vnu.edu.vn/eprints/id/eprint/2823/1/duc2017.pdf