{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,4]],"date-time":"2026-05-04T23:46:20Z","timestamp":1777938380391,"version":"3.51.4"},"reference-count":21,"publisher":"SAGE Publications","issue":"6","license":[{"start":{"date-parts":[[2020,3,4]],"date-time":"2020-03-04T00:00:00Z","timestamp":1583280000000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications"],"published-print":{"date-parts":[[2020,6]]},"abstract":"<jats:p>The present study deals with the effects of temperature and cyclic loading on the strength of single lap adhesive joints enhanced with different amounts of microcork particles. To achieve this, different joints with various overlap lengths were manufactured and tested. The joints were tested at two different temperatures (\u221220\u2009\u2103 and 75\u2009\u2103) in quasi-static conditions. Results of high temperature (75\u2009\u2103) show that the joints tensile strength decreases with the amount of cork particles. For low temperature (\u221220\u2009\u2103), the strength of the joint with 1 vol.% of cork increased; however, higher amounts of cork led to a reduction of the joint strength. To investigate the influence of cork particles on the fatigue endurance, joints were tested at room temperature under sinusoidal cyclic loading. Based on the experimental data it was found that the cork particles can significantly improve the fatigue life of adhesive joints (up to 4.6 times). Microfailure analysis of the tested joints was also performed using the scanning electron microscope technique.<\/jats:p>","DOI":"10.1177\/1464420720909848","type":"journal-article","created":{"date-parts":[[2020,3,5]],"date-time":"2020-03-05T01:23:31Z","timestamp":1583371411000},"page":"851-858","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":6,"title":["Influence of microcork particles on the lap shear strength of an epoxy adhesive subjected to fatigue loading and different environmental conditions"],"prefix":"10.1177","volume":"234","author":[{"ORCID":"https:\/\/orcid.org\/0000-0002-7168-7079","authenticated-orcid":false,"given":"Alireza","family":"Akhavan-Safar","sequence":"first","affiliation":[{"name":"Institute of Science and Innovation in Mechanical and Industrial Engineering (INEGI), Porto, Portugal"}]},{"given":"Ana Queir\u00f3s","family":"Barbosa","sequence":"additional","affiliation":[{"name":"Institute of Science and Innovation in Mechanical and Industrial Engineering (INEGI), Porto, Portugal"}]},{"ORCID":"https:\/\/orcid.org\/0000-0001-9840-6225","authenticated-orcid":false,"given":"Majid Reza","family":"Ayatollahi","sequence":"additional","affiliation":[{"name":"Fatigue and Fracture Laboratory, School of Mechanical Engineering, Iran University of Science and Technology, Tehran, Iran"}]},{"given":"Lucas Filipe Martins","family":"da Silva","sequence":"additional","affiliation":[{"name":"Department of Mechanical Engineering, Faculty of Engineering, University of Porto, Porto, Portugal"}]}],"member":"179","published-online":{"date-parts":[[2020,3,4]]},"reference":[{"key":"bibr1-1464420720909848","doi-asserted-by":"publisher","DOI":"10.1533\/9781845690755"},{"key":"bibr2-1464420720909848","doi-asserted-by":"publisher","DOI":"10.1007\/978-3-642-01169-6"},{"key":"bibr3-1464420720909848","first-page":"660","volume":"8","author":"Schroeder K","year":"1997","journal-title":"Int J Fatigue"},{"key":"bibr4-1464420720909848","doi-asserted-by":"publisher","DOI":"10.1016\/0389-4304(96)00008-2"},{"key":"bibr5-1464420720909848","unstructured":"Guyt C and Fredell R.\n                      Delamination effects in fuselage crack patching\n                      . Covina, CA: Society for the Advancement of Material and Process Engineering, 1996."},{"key":"bibr6-1464420720909848","unstructured":"Ruschau JJ and Coate JE.\n                      The effectiveness of an adhesively bonded composite patch repair as applied to a transport aircraft lower wing skin\n                      . 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