Bruyneel, M. and Degenhardt, Richard and Delsemme, J. (2009) An industrial solution to simulate post-buckling and damage of composite panels. JEC Composites Magazine, 48, pp. 38-39.
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The SAMCEF finite-element code provides solutions for modelling and analysing post-buckling in composite structures. Post-buckling results in large transversal displacements, which means that a reliable non-linear procedure is required. Ply and interface degradation models can be used to more accurately predict the complex structural behaviour of the composite structure up to the final point of collapse. This paper presents the numerical results obtained as part of research conducted under the COCOMAT European project. Comparison with experimental results shows that SAMCEF accurately predicts the damage mechanisms, panel behaviour and collapse load.
|Title:||An industrial solution to simulate post-buckling and damage of composite panels|
|Journal or Publication Title:||JEC Composites Magazine|
|In ISI Web of Science:||No|
|Page Range:||pp. 38-39|
|Keywords:||post-buckling, damage, composite|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Structural Mechanics|
|Deposited By:||Doris Ries|
|Deposited On:||15 Feb 2010 12:22|
|Last Modified:||07 Feb 2013 20:07|
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