Full metadata record
DC FieldValueLanguage
dc.contributor.authorKottner, Radek
dc.contributor.authorBek, Lukáš
dc.contributor.authorKrystek, Jan
dc.contributor.authorKroft, Roman
dc.date.accessioned2020-11-16T11:00:18Z-
dc.date.available2020-11-16T11:00:18Z-
dc.date.issued2020
dc.identifier.citationKOTTNER, R., BEK, L., KRYSTEK, J., KROFT, R. Failure of Blind Riveted Joint of Carbon Laminates. In: AIAA Scitech 2020 Forum. Neuveden: American Institute of Aeronautics and Astronautics Inc, AIAA, 2020. s. 1-18. ISBN 978-1-62410-595-1.cs
dc.identifier.isbn978-1-62410-595-1
dc.identifier.uri2-s2.0-85092352867
dc.identifier.urihttp://hdl.handle.net/11025/41903
dc.format18 s.
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherAmerican Institute of Aeronautics and Astronautics Inc, AIAAen
dc.relation.ispartofseriesAIAA Scitech 2020 Forumen
dc.rightsPlný text není přístupný.cs
dc.rights© American Institute of Aeronautics and Astronauticsen
dc.titleFailure of Blind Riveted Joint of Carbon Laminatesen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.rights.accessclosedAccessen
dc.type.versionpublishedVersionen
dc.description.abstract-translatedThispaperdealswiththeexperimentalandnumericalinvestigationsofmechanicalbehavior of the single-lap joint of laminates consisting of TENAX-J IMS60 E13 24K carbon fibers and MSG L285 epoxy resin. TIBULB high-strength blind rivets having a diameter of 4.8 mm and 6.4 mm were used for the joint. Tension tests were performed to investigate the material parameters of the laminate and the clearance effect. The rivet clamping force was evaluated based on a torsion test. The finite element method model of the joint using non-linear shear stress-strain relations of a lamina and using Puck’s failure criterion for the 3D stress state was created. The model was used to analyze the failure of the joint under quasi-static loading. The maximum number of loading cycles leading to joint failure and the decrease in the joint load capacity and stiffness due to the cyclic loading were investigated.en
dc.subject.translatedBlind riveted jointen
dc.subject.translatedfatigueen
dc.subject.translatedclearanceen
dc.subject.translatedfailureen
dc.subject.translatedcompositeen
dc.identifier.doi10.2514/6.2020-1931
dc.type.statusPeer-revieweden
dc.identifier.obd43928626
dc.project.IDEF17_048/0007267/InteCom: VaV inteligentních komponent pokročilých technologií pro plzeňskou metropolitní oblastcs
dc.project.IDLO1506/PUNTIS - Podpora udržitelnosti centra NTIS - Nové technologie pro informační společnostcs
Appears in Collections:Konferenční příspěvky / Conference papers (NTIS)
OBD

Files in This Item:
File SizeFormat 
kottner_SciTech2020.pdf8,53 MBAdobe PDFView/Open    Request a copy


Please use this identifier to cite or link to this item: http://hdl.handle.net/11025/41903

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

search
navigation
  1. DSpace at University of West Bohemia
  2. Publikační činnost / Publications
  3. OBD