contributor author | A. Chakrabarti | |
contributor author | A. H. Sheikh | |
date accessioned | 2017-05-08T21:16:10Z | |
date available | 2017-05-08T21:16:10Z | |
date copyright | July 2004 | |
date issued | 2004 | |
identifier other | %28asce%290893-1321%282004%2917%3A3%28123%29.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45006 | |
description abstract | An efficient six-noded triangular element based on refined plate theory is developed for the analysis of sandwich plates with stiff laminated face sheets and it is applied to a free vibration problem in this paper. The plate theory represents parabolic through thickness variation of transverse shear stresses with continuity at the layer interfaces, which introduces discontinuity at these interfaces for the shear strains. It is to be noted that the plate theory requires unknowns at the reference plane only. Moreover, it ensures a shear stress-free condition at the top and bottom surfaces of the plate. Thus, the plate theory has all of the features required for an accurate modeling of laminated sandwich plates. The plate theory suffers from a problem in its finite element implementation since it requires | |
publisher | American Society of Civil Engineers | |
title | Vibration of Laminate-Faced Sandwich Plate by a New Refined Element | |
type | Journal Paper | |
journal volume | 17 | |
journal issue | 3 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)0893-1321(2004)17:3(123) | |
tree | Journal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003 | |
contenttype | Fulltext | |