Change of strain field due to damage development in adhesive joints

In this thesis six metal I-beams with a crack repaired by a composite patch been tested in four point bending. The patches used to repair the beams had three different patch thicknesses. The different thicknesses were manufactured to see how the thickness affects the stress field inside the laminate...

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Main Author: Midtbø, Carl-Magnus
Format: Others
Language:English
Published: Norges teknisk-naturvitenskapelige universitet, Institutt for produktutvikling og materialer 2013
Online Access:http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-24285
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spelling ndltd-UPSALLA1-oai-DiVA.org-ntnu-242852014-03-13T04:42:03ZChange of strain field due to damage development in adhesive jointsengMidtbø, Carl-MagnusNorges teknisk-naturvitenskapelige universitet, Institutt for produktutvikling og materialerInstitutt for produktutvikling og materialer2013In this thesis six metal I-beams with a crack repaired by a composite patch been tested in four point bending. The patches used to repair the beams had three different patch thicknesses. The different thicknesses were manufactured to see how the thickness affects the stress field inside the laminates. To attach the patch to the steel beam, adhesive joints were used. However, the long-term performances of such joints are still not well understood. Monitoring the damage development in joints like this can provide a better understanding of how the damage propagates to investigate the long-term performance of the joint. A new method using optical fibers to measure strains inside the laminates was used. It is possible to measure the strains in different layers of the laminate by using optical fibers. Compared to traditional strain gauges which measures strain in a small area, the optical fibers can measure a length up to 70 meters. All of the beams have been monitored with seven traditional electrical strain gauges and up to eight optical fibers. The measurements done with the optical fibers made it possible to plot the changes of the strain field due to damage development inside the laminate through the thickness. It is concluded that the strain field over the notch in a given layer inside laminate, has the same shape independent of thickness. This thesis also confirms that the angle of the tapering at the end of the laminate has an impact on where the laminate starts to delaminate. Typically, the delamination starts at the highest strain concentration, either at the notch or one side of the laminate. It has also been possible to use the shape of the strain field to predict approximately how far the delamination has propagated. Student thesisinfo:eu-repo/semantics/bachelorThesistexthttp://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-24285Local ntnudaim:10440application/pdfinfo:eu-repo/semantics/openAccess
collection NDLTD
language English
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description In this thesis six metal I-beams with a crack repaired by a composite patch been tested in four point bending. The patches used to repair the beams had three different patch thicknesses. The different thicknesses were manufactured to see how the thickness affects the stress field inside the laminates. To attach the patch to the steel beam, adhesive joints were used. However, the long-term performances of such joints are still not well understood. Monitoring the damage development in joints like this can provide a better understanding of how the damage propagates to investigate the long-term performance of the joint. A new method using optical fibers to measure strains inside the laminates was used. It is possible to measure the strains in different layers of the laminate by using optical fibers. Compared to traditional strain gauges which measures strain in a small area, the optical fibers can measure a length up to 70 meters. All of the beams have been monitored with seven traditional electrical strain gauges and up to eight optical fibers. The measurements done with the optical fibers made it possible to plot the changes of the strain field due to damage development inside the laminate through the thickness. It is concluded that the strain field over the notch in a given layer inside laminate, has the same shape independent of thickness. This thesis also confirms that the angle of the tapering at the end of the laminate has an impact on where the laminate starts to delaminate. Typically, the delamination starts at the highest strain concentration, either at the notch or one side of the laminate. It has also been possible to use the shape of the strain field to predict approximately how far the delamination has propagated.
author Midtbø, Carl-Magnus
spellingShingle Midtbø, Carl-Magnus
Change of strain field due to damage development in adhesive joints
author_facet Midtbø, Carl-Magnus
author_sort Midtbø, Carl-Magnus
title Change of strain field due to damage development in adhesive joints
title_short Change of strain field due to damage development in adhesive joints
title_full Change of strain field due to damage development in adhesive joints
title_fullStr Change of strain field due to damage development in adhesive joints
title_full_unstemmed Change of strain field due to damage development in adhesive joints
title_sort change of strain field due to damage development in adhesive joints
publisher Norges teknisk-naturvitenskapelige universitet, Institutt for produktutvikling og materialer
publishDate 2013
url http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-24285
work_keys_str_mv AT midtbøcarlmagnus changeofstrainfieldduetodamagedevelopmentinadhesivejoints
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