eprintid: 1208
rev_number: 4
eprint_status: archive
userid: 5
dir: disk0/00/00/12/08
datestamp: 2015-08-05 04:43:30
lastmod: 2015-08-05 04:43:30
status_changed: 2015-08-05 04:43:30
type: article
metadata_visibility: show
creators_name: Nguyen, Dinh Duc
creators_name: Pham, Toan Thang
creators_id: ducnd@vnu.edu.vn
title: Nonlinear dynamic response and vibration of shear deformable imperfect eccentrically stiffened S-FGM circular cylindrical shells surrounded on elastic foundations
ispublished: pub
divisions: fac_fema
abstract: This paper presents an analytical approach to investigate the nonlinear dynamic response and vibration of imperfect eccentrically stiffened functionally graded thick circular cylindrical shells surrounded on elastic foundations using both the first order shear deformation theory and stress function with full motion equations (not using Volmir's assumptions). Material properties are graded in the thickness direction according to a sigmoid power law distribution (S-FGM) in terms of the volume fractions of constituents with metal–ceramic–metal layers. The S-FGM shells are subjected to mechanical and damping loads. Numerical results for dynamic response of the shells are obtained by Runge–Kutta method. The results show the influences of geometrical parameters, the volume fractions of metal–ceramic–metal layers, imperfections, the elastic foundations, eccentrically stiffeners, pre-loaded axial compression and damping loads on the nonlinear dynamic response and nonlinear vibration of functionally graded cylindrical shells. The proposed results are validated by comparing with other results reported in the literature.
date: 2015-01
date_type: published
official_url: doi:10.1016/j.ast.2014.11.005
full_text_status: none
publication: Aerospace Science and Technology Volume 40, January 2015, Pages 115–127
volume: 40
pagerange: 115-127
refereed: TRUE
citation:   Nguyen, Dinh Duc and Pham, Toan Thang  (2015) Nonlinear dynamic response and vibration of shear deformable imperfect eccentrically stiffened S-FGM circular cylindrical shells surrounded on elastic foundations.  Aerospace Science and Technology Volume 40, January 2015, Pages 115–127, 40 .   pp. 115-127.