{"data":{"id":"10.4121/uuid:1495c951-33e2-43ab-9f41-5ed3b57ba02f","type":"dois","attributes":{"doi":"10.4121/uuid:1495c951-33e2-43ab-9f41-5ed3b57ba02f","prefix":"10.4121","suffix":"uuid:1495c951-33e2-43ab-9f41-5ed3b57ba02f","identifiers":[],"alternateIdentifiers":[],"creators":[{"name":"Pascoe, John-Alan","nameType":"Personal","givenName":"John-Alan","familyName":"Pascoe","nameIdentifiers":[{"nameIdentifier":"0000-0003-2771-8285","nameIdentifierScheme":"https://orcid.org/"}],"affiliation":[]},{"name":"Al Amery, A. M.K. H. (Ali)","givenName":"A. M.K. H. (Ali)","familyName":"Al Amery","affiliation":[],"nameIdentifiers":[]},{"name":"Zavatta, N. (Nicola)","givenName":"N. (Nicola)","familyName":"Zavatta","affiliation":[],"nameIdentifiers":[]}],"titles":[{"title":"Effect of Bondline Thickness on Fatigue Crack Growth in FM94"}],"publisher":"TU Delft","container":{},"publicationYear":2016,"subjects":[{"subject":"Aerospace Engineering","subjectScheme":"Australian and New Zealand Standard Research Classification (ANZSRC), 2008","classificationCode":"0901"},{"subject":"FOS: Mechanical engineering","schemeUri":"http://www.oecd.org/science/inno/38235147.pdf","subjectScheme":"Fields of Science and Technology (FOS)"},{"subject":"Adhesive bond"},{"subject":"Aerospace engineering"},{"subject":"Bonded joint"},{"subject":"Double Cantilever Beam (DCB)"},{"subject":"Double cantilever beam"},{"subject":"Epoxy"},{"subject":"FM94"},{"subject":"Fatigue crack growth"},{"subject":"Glass-Fibre Reinforced Polymer (GFRP)"},{"subject":"Glass-fibre reinforced polymer"},{"subject":"Mode I"},{"subject":"dissertation"}],"contributors":[{"name":"Alderliesten, R.C. (René)","nameType":"Personal","affiliation":[],"contributorType":"Other","nameIdentifiers":[{"nameIdentifier":"0000-0003-1882-5396","nameIdentifierScheme":"https://orcid.org/"}]},{"name":"Benedictus, R. (Rinze)","nameType":"Personal","affiliation":[],"contributorType":"Other","nameIdentifiers":[{"nameIdentifier":"0000-0003-3219-3161","nameIdentifierScheme":"https://orcid.org/"}]},{"name":"Delft University Of Technology-Faculty Of Aerospace Engineering","nameType":"Organizational","affiliation":[],"contributorType":"Other","nameIdentifiers":[]}],"dates":[{"date":"2016-06-08","dateType":"Issued"}],"language":"en","types":{"ris":"DATA","bibtex":"misc","citeproc":"dataset","schemaOrg":"Dataset","resourceType":"Dataset","resourceTypeGeneral":"Dataset"},"relatedIdentifiers":[{"relationType":"References","relatedIdentifier":"https://doi.org/10.1016/j.engfracmech.2020.106959","relatedIdentifierType":"URL"},{"relationType":"References","relatedIdentifier":"http://amslaurea.unibo.it/9713/1/zavatta_nicola_tesi.pdf.pdf","relatedIdentifierType":"URL"},{"relationType":"References","relatedIdentifier":"https://doi.org/10.4233/uuid:ebbf552a-ce98-4ab6-b9cc-0b939e12ba8b","relatedIdentifierType":"URL"},{"relationType":"References","relatedIdentifier":"https://doi.org/10.4121/uuid:4400f37c-7168-4275-a778-09b237bd34c6","relatedIdentifierType":"URL"}],"relatedItems":[],"sizes":[],"formats":["media types: application/octet-stream, application/pdf, application/zip, text/csv, text/plain"],"version":"1","rightsList":[{"rights":"4TU General Terms of Use","rightsUri":"https://doi.org/10.4121/resource:terms_of_use"}],"descriptions":[{"description":"Fatigue crack growth experiments on aluminium-2024-T3 / FM94 epoxy / aluminium-2024-T3 bonded joint specimens in the double cantilever beam (DCB) configuration. Different adhesive thicknesses were tested. Also contains data from fatigue crack growth experiments conducted on S2-glass / FM94 epoxy composite laminates again in the DCB configuration. Different fibre orientations were tested. Included data are raw data: crack length, force, and displacement measurements, as well as processed data such as strain energy release rates and energy dissipation per 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