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Statements

Subject Item
n2:RIV%2F68407700%3A21110%2F14%3A00214192%21RIV15-MSM-21110___
rdf:type
n5:Vysledek skos:Concept
rdfs:seeAlso
http://arxiv.org/abs/1303.6314
dcterms:description
Laminated glass structures are formed by stiff layers of glass connected with a compliant plastic interlayer. Due to their slenderness and heterogeneity, they exhibit a complex mechanical response that is difficult to capture by single-layer models even in the elastic range. The purpose of this paper is to introduce an efficient and reliable finite element approach to the simulation of the immediate response of laminated glass beams. It proceeds from a refined plate theory due to Mau (1973), as we treat each layer independently and enforce the compatibility by the Lagrange multipliers. At the layer level, we adopt the finite-strain shear deformable formulation of Reissner (1972) and the numerical framework by Ibrahimbegovic and Frey (1993). The resulting system is solved by the Newton method with consistent linearization. By comparing the model predictions against available experimental data, analytical methods and two-dimensional finite element simulations, we demonstrate that the proposed formulation is reliable and provides accuracy comparable to the detailed two-dimensional finite element analyzes. As such, it offers a convenient basis to incorporate more refined constitutive description of the interlayer. Laminated glass structures are formed by stiff layers of glass connected with a compliant plastic interlayer. Due to their slenderness and heterogeneity, they exhibit a complex mechanical response that is difficult to capture by single-layer models even in the elastic range. The purpose of this paper is to introduce an efficient and reliable finite element approach to the simulation of the immediate response of laminated glass beams. It proceeds from a refined plate theory due to Mau (1973), as we treat each layer independently and enforce the compatibility by the Lagrange multipliers. At the layer level, we adopt the finite-strain shear deformable formulation of Reissner (1972) and the numerical framework by Ibrahimbegovic and Frey (1993). The resulting system is solved by the Newton method with consistent linearization. By comparing the model predictions against available experimental data, analytical methods and two-dimensional finite element simulations, we demonstrate that the proposed formulation is reliable and provides accuracy comparable to the detailed two-dimensional finite element analyzes. As such, it offers a convenient basis to incorporate more refined constitutive description of the interlayer.
dcterms:title
Numerical model of elastic laminated glass beams under finite strain Numerical model of elastic laminated glass beams under finite strain
skos:prefLabel
Numerical model of elastic laminated glass beams under finite strain Numerical model of elastic laminated glass beams under finite strain
skos:notation
RIV/68407700:21110/14:00214192!RIV15-MSM-21110___
n4:aktivita
n13:S n13:P
n4:aktivity
P(ED1.1.00/02.0070), P(GAP105/11/0224), P(GAP105/12/0331), S
n4:cisloPeriodika
4
n4:dodaniDat
n11:2015
n4:domaciTvurceVysledku
n9:4695046 n9:2342448 n9:3638464
n4:druhVysledku
n14:J
n4:duvernostUdaju
n16:S
n4:entitaPredkladatele
n7:predkladatel
n4:idSjednocenehoVysledku
33299
n4:idVysledku
RIV/68407700:21110/14:00214192
n4:jazykVysledku
n10:eng
n4:klicovaSlova
laminated glass; finite-strain Reissner beam theory; finite element method; Lagrange multipliers
n4:klicoveSlovo
n6:laminated%20glass n6:finite-strain%20Reissner%20beam%20theory n6:Lagrange%20multipliers n6:finite%20element%20method
n4:kodStatuVydavatele
NL - Nizozemsko
n4:kontrolniKodProRIV
[39CCA44B27F3]
n4:nazevZdroje
Archives of Civil and Mechanical Engineering
n4:obor
n18:JN
n4:pocetDomacichTvurcuVysledku
3
n4:pocetTvurcuVysledku
3
n4:projekt
n15:GAP105%2F12%2F0331 n15:GAP105%2F11%2F0224 n15:ED1.1.00%2F02.0070
n4:rokUplatneniVysledku
n11:2014
n4:svazekPeriodika
14
n4:tvurceVysledku
Zemanová, Alena Šejnoha, Michal Zeman, Jan
n4:wos
000344517300023
s:issn
1644-9665
s:numberOfPages
11
n20:doi
10.1016/j.acme.2014.03.005
n19:organizacniJednotka
21110