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:

Authors	Institution or Email of Authors
Johnson, Alastair
Toso-Pentecote, Nathalie
Schwinn, Dominik

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

HGF - Program:

Aeronautics

HGF - Program Themes:

L AR - 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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