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dc.contributor.authorSoltannia, Babak
dc.date.accessioned2013-08-27T19:01:27Z
dc.date.available2013-08-27T19:01:27Z
dc.date.issued2013-08-27
dc.identifier.urihttp://hdl.handle.net/10222/36272
dc.description.abstractThe effects of high loading rates (HLR), and nano reinforcement on the mechanical response of adhesively-bonded SLJs with composite adherends, subjected to different loading (strain) rates are systematically investigated. The results are then compared to those of neat thermoset resin and thermo-plastic adhesive. More specifically, nano-reinforced and neat resin bonded joints mating carbon/epoxy and glass/epoxy adherends were subjected to tensile loadings under 1.5 and 3 mm/min and tensile impacts at a loading rate of 2.04E+5 mm/min. In some cases, additional tests were conducted under 15, 150, and 1500 mm/min to obtain additional properties gained using the nano-reinforcements for use in the further numerical investigations. The HLR tests were conducted, using a modified instrumented pendulum equipped with a specially designed impact load transfer apparatus. The dispersion of nanoparticles was facilitated using a mechanical stirrer and a three-roll mill machine. The failure mechanisms were studied with a scanning electron microscope.en_US
dc.language.isoenen_US
dc.subjectAdhesively bonded joints; Single-lap joints; Graphene nanoplatelets; Nano composites; Loading rate; High loading rate.en_US
dc.titleCHARACTERIZATION OF NANOCARBON-REINFORCED AND NEAT ADHESIVES IN BONDED SINGLE LAP JOINTS UNDER STATIC AND IMPACT LOADINGSen_US
dc.date.defence2013-08-16
dc.contributor.departmentDepartment of Civil Engineeringen_US
dc.contributor.degreeMaster of Applied Scienceen_US
dc.contributor.external-examinerDr. Malcolm Smithen_US
dc.contributor.graduate-coordinatorDr. Lei Liuen_US
dc.contributor.thesis-readerProfessor Tamunoiyala Kokoen_US
dc.contributor.thesis-supervisorProfessor Farid Taherien_US
dc.contributor.ethics-approvalNot Applicableen_US
dc.contributor.manuscriptsYesen_US
dc.contributor.copyright-releaseNot Applicableen_US
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