Mechanical behavior after repairing structure by fiber carbon
Abstract: In this paper, an analytic study is presented to investigate the effect of crack length on the single-lap shear joint under tensile load and to analyze the distribution of adhesive shear stress. A parametric study was conducted in accordance with changes in dimensions of the pre-crack posi...
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Escuela de Construcción Civil, Pontificia Universidad Católica de Chile
2017
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oai:scielo:S0718-915X20170003004122018-03-05Mechanical behavior after repairing structure by fiber carbonAyad,TayebKadri,TaharRezigua,Ahmed composite shear stress bonded assembly crack structure. Abstract: In this paper, an analytic study is presented to investigate the effect of crack length on the single-lap shear joint under tensile load and to analyze the distribution of adhesive shear stress. A parametric study was conducted in accordance with changes in dimensions of the pre-crack position to evaluate shear stress along the bonded joint. A finite element analysis (FEA) was proposed for validation of our analytic model and for determination of stress concentration points of the pre-crack and the two edges of the bonded assembly. Results in this paper show good agreement between analytic study and the FEA model for shear stress at both free edges of adhesive.info:eu-repo/semantics/openAccessEscuela de Construcción Civil, Pontificia Universidad Católica de ChileRevista de la construcción v.16 n.3 20172017-09-01text/htmlhttp://www.scielo.cl/scielo.php?script=sci_arttext&pid=S0718-915X2017000300412en10.7764/rdlc.16.3.412 |
institution |
Scielo Chile |
collection |
Scielo Chile |
language |
English |
topic |
composite shear stress bonded assembly crack structure. |
spellingShingle |
composite shear stress bonded assembly crack structure. Ayad,Tayeb Kadri,Tahar Rezigua,Ahmed Mechanical behavior after repairing structure by fiber carbon |
description |
Abstract: In this paper, an analytic study is presented to investigate the effect of crack length on the single-lap shear joint under tensile load and to analyze the distribution of adhesive shear stress. A parametric study was conducted in accordance with changes in dimensions of the pre-crack position to evaluate shear stress along the bonded joint. A finite element analysis (FEA) was proposed for validation of our analytic model and for determination of stress concentration points of the pre-crack and the two edges of the bonded assembly. Results in this paper show good agreement between analytic study and the FEA model for shear stress at both free edges of adhesive. |
author |
Ayad,Tayeb Kadri,Tahar Rezigua,Ahmed |
author_facet |
Ayad,Tayeb Kadri,Tahar Rezigua,Ahmed |
author_sort |
Ayad,Tayeb |
title |
Mechanical behavior after repairing structure by fiber carbon |
title_short |
Mechanical behavior after repairing structure by fiber carbon |
title_full |
Mechanical behavior after repairing structure by fiber carbon |
title_fullStr |
Mechanical behavior after repairing structure by fiber carbon |
title_full_unstemmed |
Mechanical behavior after repairing structure by fiber carbon |
title_sort |
mechanical behavior after repairing structure by fiber carbon |
publisher |
Escuela de Construcción Civil, Pontificia Universidad Católica de Chile |
publishDate |
2017 |
url |
http://www.scielo.cl/scielo.php?script=sci_arttext&pid=S0718-915X2017000300412 |
work_keys_str_mv |
AT ayadtayeb mechanicalbehaviorafterrepairingstructurebyfibercarbon AT kadritahar mechanicalbehaviorafterrepairingstructurebyfibercarbon AT reziguaahmed mechanicalbehaviorafterrepairingstructurebyfibercarbon |
_version_ |
1714206285875904512 |