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Modelling damage in composite aircraft panels under tyre rubber impacts

Johnson, Alastair and Toso-Pentecote, Nathalie and Schwinn, Dominik (2009) Modelling damage in composite aircraft panels under tyre rubber impacts. In: Conference Proceedings. ICCM17 (17th International Conference on Composite Materials, 27-31 Jul. 2009, Edinburgh, UK.

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Abstract

The paper uses meso-scale composites ply damage models with an energy based delamination failurecriteria in an explicit FE code to study damage progression in composite panels under impact. A study is made of damage in frame stiffened aircraft panels and a composite wing lower cover panel impacted by tyre fragments.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Modelling damage in composite aircraft panels under tyre rubber impacts
Authors:
AuthorsInstitution or Email of Authors
Johnson, AlastairUNSPECIFIED
Toso-Pentecote, NathalieUNSPECIFIED
Schwinn, DominikUNSPECIFIED
Date:July 2009
Journal or Publication Title:Conference Proceedings
Status:Published
Keywords:composite damage, delamination models, FE code developments, stiffened aircraft panels, simulation of impact damage
Event Title:ICCM17 (17th International Conference on Composite Materials
Event Location:Edinburgh, UK
Event Type:international Conference
Event Dates:27-31 Jul. 2009
Organizer:The British Composites Society
HGF - Research field:Aeronautics, Space and Transport (old)
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
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Deposited By: Nathalie Toso
Deposited On:04 Dec 2009 17:16
Last Modified:04 Dec 2009 17:16

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