Title:	Failure of Blind Riveted Joint of Carbon Laminates
Authors:	Kottner, Radek Bek, Lukáš Krystek, Jan Kroft, Roman
Citation:	KOTTNER, 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.
Issue Date:	2020
Publisher:	American Institute of Aeronautics and Astronautics Inc, AIAA
Document type:	konferenční příspěvek conferenceObject
URI:	2-s2.0-85092352867 http://hdl.handle.net/11025/41903
ISBN:	978-1-62410-595-1
Keywords in different language:	Blind riveted joint;fatigue;clearance;failure;composite
Abstract in different language:	Thispaperdealswiththeexperimentalandnumericalinvestigationsofmechanicalbehavior 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.
Rights:	Plný text není přístupný. © American Institute of Aeronautics and Astronautics
Appears in Collections:	Konferenční příspěvky / Conference papers (NTIS) OBD

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