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contributor authorPratik Tiwari
contributor authorSwarup K. Barman
contributor authorDipak K. Maiti
contributor authorDamodar Maity
date accessioned2019-09-18T10:40:48Z
date available2019-09-18T10:40:48Z
date issued2019
identifier other%28ASCE%29AS.1943-5525.0001053.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4260196
description abstractIn this study, a new model for analyzing delaminated plates was developed using three-dimensional (3D) degenerated elements. The elements were developed using the degenerated solid approach based on Reissner-Mindlin assumptions. Thus, the shear deformation and rotary inertia effect were considered, and the 3D field was reduced to a two-dimensional (2D) field in terms of midsurface nodal variables. The delamination was incorporated using Heaviside step functions. The proposed model was found to be very accurate and also faster in comparison with layerwise/higher-order theories. Results for natural frequencies of plates and beams with and without delamination were compared with theoretical and experimental results available in the literature and were in excellent agreement. New results were generated using the proposed method for different boundary conditions, ply orientations, size of delamination, and location of delamination; these will serve as benchmarks for future research.
publisherAmerican Society of Civil Engineers
titleFree Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element
typeJournal Paper
journal volume32
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001053
page04019070
treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
contenttypeFulltext


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