{"title":"Numerical Prediction of Bearing Strength on Composite Bolted Joint Using Three Dimensional Puck Failure Criteria","authors":"M. S. Meon, M. N. Rao, K-U. Schr\u00f6der","volume":118,"journal":"International Journal of Materials and Metallurgical Engineering","pagesStart":1281,"pagesEnd":1287,"ISSN":"1307-6892","URL":"https:\/\/publications.waset.org\/pdf\/10005548","abstract":"Mechanical fasteners especially bolting is commonly
\r\nused in joining carbon-fiber reinforced polymer (CFRP) composite
\r\nstructures due to their good joinability and easy for maintenance
\r\ncharacteristics. Since this approach involves with notching, a proper
\r\nprogressive damage model (PDM) need to be implemented and
\r\nverified to capture existence of damages in the structure. A three
\r\ndimensional (3D) failure criteria of Puck is established to predict the
\r\nultimate bearing failure of such joint. The failure criteria incorporated
\r\nwith degradation scheme are coded based on user subroutine executed
\r\nin Abaqus. Single lap joint (SLJ) of composite bolted joint is used as
\r\ntarget configuration. The results revealed that the PDM adopted here
\r\ncould sufficiently predict the behaviour of composite bolted joint up
\r\nto ultimate bearing failure. In addition, mesh refinement near holes
\r\nincreased the accuracy of predicted strength as well as computational
\r\neffort.","references":"[1] Y. Liu, B. Zwingmann, and M. Schlaich, \u201cNonlinear progressive damage\r\nanalysis of notched or bolted fibre-reinforced polymer (FRP) laminates\r\nbased on a three-dimensional strain failure criterion,\u201d Polymers, vol. 6,\r\nno. 4, pp. 949\u2013976, 2014. [2] M. V. Donadon, S. F. M. De Almeida, M. A. Arbelo, and A. R. de Faria,\r\n\u201cA three-dimensional ply failure model for composite structures,\u201d\r\nInternational Journal of Aerospace Engineering, vol. 2009, 2009.\r\n[3] K. Rohwer, \u201cPredicting fibre composite damage and failure,\u201d Journal of\r\nComposite Materials, vol. 49, no. 21, pp. 2673\u20132683, 2015.\r\n[4] O. O. Ochoa and J. N. Reddy, Finite Element Analysis of Composite\r\nLaminates. Dordrecht: Springer Netherlands, 1992, ch. Finite Element\r\nAnalysis of Composite Laminates, pp. 37\u2013109.\r\n[5] N. F. Knight Jr and J. R. 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