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contributor authorA. Chakrabarti
contributor authorA. H. Sheikh
date accessioned2017-05-08T21:16:10Z
date available2017-05-08T21:16:10Z
date copyrightJuly 2004
date issued2004
identifier other%28asce%290893-1321%282004%2917%3A3%28123%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45006
description abstractAn 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
publisherAmerican Society of Civil Engineers
titleVibration of Laminate-Faced Sandwich Plate by a New Refined Element
typeJournal Paper
journal volume17
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2004)17:3(123)
treeJournal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003
contenttypeFulltext


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