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Residual Strength of In-Plane Loaded Debonded Sandwich Panels: Fracture Mechanical Modelling
Abstract This paper presents a FEM based numerical model for prediction of residual strength of damaged sandwich panels. As demonstrated, the model can predict the maximum load carrying capacity of real-life panels with debond damages, where the failure is governed by face-sheet buckling followed by debond growth. Comparison of the theoretical predictions is carried out against a series of large-scale experiments described in Lundsgaard-Larsen et al. [1].
Residual Strength of In-Plane Loaded Debonded Sandwich Panels: Fracture Mechanical Modelling
Abstract This paper presents a FEM based numerical model for prediction of residual strength of damaged sandwich panels. As demonstrated, the model can predict the maximum load carrying capacity of real-life panels with debond damages, where the failure is governed by face-sheet buckling followed by debond growth. Comparison of the theoretical predictions is carried out against a series of large-scale experiments described in Lundsgaard-Larsen et al. [1].
Residual Strength of In-Plane Loaded Debonded Sandwich Panels: Fracture Mechanical Modelling
Berggreen, Christian (author) / Simonsen, Bo Cerup (author)
2005-01-01
10 pages
Article/Chapter (Book)
Electronic Resource
English
Residual strength of in-plane loaded debonded sandwich panels. Fracture mechanical modelling
British Library Conference Proceedings | 2005
|Residual strength of in-plane loaded debonded sandwich panels. Experimental investigation
British Library Conference Proceedings | 2005
|Residual Strength of In-Plane Loaded Debonded Sandwich Panels: Experimental Investigation
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|Residual strength of debonded sandwich panels loaded with lateral pressure
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