| People | Locations | Statistics |
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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Branner, Kim
Technical University of Denmark
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (26/26 displayed)
- 2025Acoustic emission data analytics on delamination growth in a wind turbine blade under full-scale cyclic testingcitations
- 2024Monitoring Damage Progression in Wind Turbine Blade Under Fatigue Testing Using Acceleration Measurements
- 2024Monitoring Damage Progression in Wind Turbine Blade Under Fatigue Testing Using Acceleration Measurements
- 2021Optimized method for multi-axial fatigue testing of wind turbine bladescitations
- 2021Fatigue testing of a 14.3 m composite blade embedded with artificial defects – damage growth and structural health monitoringcitations
- 2019Understanding progressive failure mechanisms of a wind turbine blade trailing edge section through subcomponent tests and nonlinear FE analysiscitations
- 2018Assessment and propagation of mechanical property uncertainties in fatigue life prediction of composite laminatescitations
- 2018Buckling and progressive failure of trailing edge subcomponent of wind turbine blade
- 2016Methodology for testing subcomponents; background and motivation for subcomponent testing of wind turbine rotor blades
- 2015New morphing blade section designs and structural solutions for smart blades
- 2015Effect of Trailing Edge Damage on Full-Scale Wind Turbine Blade Failure
- 2015Comparing Fatigue Life Estimations of Composite Wind Turbine Blades using different Fatigue Analysis Tools
- 2014Advanced topics on rotor blade full-scale structural fatigue testing and requirements
- 2014An high order Mixed Interpolation Tensorial Components (MITC) shell element approach for modeling the buckling behavior of delaminated compositescitations
- 2014Strain and displacement controls by fibre bragg grating and digital image correlationcitations
- 2014Uncertainty Quantification in Experimental Structural Dynamics Identification of Composite Material Structures
- 2013Calibration of a finite element composite delamination model by experiments
- 2012Experimental Determination and Numerical Modelling of Process Induced Strains and Residual Stresses in Thick Glass/Epoxy Laminate
- 2012Experimental Determination and Numerical Modelling of Process Induced Strains and Residual Stresses in Thick Glass/Epoxy Laminate
- 2011Finite elements modeling of delaminations in composite laminates
- 2011Compressive strength of thick composite panels
- 2010Full Scale Test of SSP 34m blade, edgewise loading LTT:Data Report 1
- 2008Full Scale Test of a SSP 34m boxgirder 2:Data report
- 2008Buckling Strength of Thick Composite Panels in Wind Turbine Blades
- 2008Buckling Strength of Thick Composite Panels in Wind Turbine Blades
- 2008Full Scale Test of a SSP 34m boxgirder 2
Places of action
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document
Finite elements modeling of delaminations in composite laminates
Abstract
The application of composite materials in many structures poses to engineers the problem to create reliable and relatively simple methods, able to estimate the strength of multilayer composite structures. Multilayer composites, like other laminated materials, suffer from layer separation, i.e., delaminations, which may affect the stiffness and stability of structural components. Especially deep delaminations in the mid surface of laminates are expected to reduce the effective flexural stiffness and lead to collapse, often due to buckling behaviour. This paper deals with the numerical modelling of the buckling strength of composite laminates containing delaminations. Namely, non-linear buckling and post-buckling analyses are carried out to predict the critical buckling load of elementary composite laminates affected by rectangular delaminations of different sizes and locations, which are modelled by finite elements using different techniques. Results obtained with different finite element models are compared and discussed.