Pearce, Garth and Johnson, Alastair and Thomson, Rodney and Kelly, Don (2010) Numerical investigation of dynamically loaded bolted joints in carbon fibre composite structures. Applied Composite Materials, 17 (3), pp. 329-346. Springer. DOI: 10.1007/s10443-009-9123-5.
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This paper presents quasi-static and dynamic modelling of bolted composite structures using the explicit finite element code PAM-CRASH. User controlled point link (PLINK) elements were investigated for modelling the bolted composite joints used in the structures. Simulation results were compared with quasi-static and dynamic structural testing reported previously. Two loading configurations were considered. It was shown that the PLINK element modelling approach agreed well with the experimental results for both loading configurations and for one case offered significant improvements over other simplified bolt modelling methods. A stacked shell modelling approach was used to model the interlaminar delamination damage present in the ball-loaded impact mode. The overall response of the structure was significantly improved by the addition of these energy absorbing interfaces.
|Title:||Numerical investigation of dynamically loaded bolted joints in carbon fibre composite structures|
|Journal or Publication Title:||Applied Composite Materials|
|In Open Access:||No|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 329-346|
|Keywords:||Carbon fibre composites, Polymer matrix composites, Bolted joints, Impact modelling, Explicit finite element analysis.|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Rotorcraft|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L RR - Rotorcraft Research|
|DLR - Research theme (Project):||L - The Robust Rotorcraft|
|Institutes and Institutions:||Institute of Structures and Design > Structural Integrity|
|Deposited By:||Dr.phil. Alastair Johnson|
|Deposited On:||09 Jan 2011 18:03|
|Last Modified:||07 Feb 2013 20:43|
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