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Modelling Damage in Stiffened Composite Panels under High Velocity Impact

Toso-Pentecote, Nathalie and Johnson, Alastair (2010) Modelling Damage in Stiffened Composite Panels under High Velocity Impact. IACM. ECCM 2010: IV European Conference on Computational Mechanics, 16-21 May 2010, Paris, France.

Full text not available from this repository.

Abstract

The paper uses meso-scale composites damage models in explicit FE codes to study damage progression in composite structures under impact. Focus in the paper is the prediction of damage progression in stringer stiffened composite shells due to impact from metal objects and tyre rubber fragments, with gas gun test data on panel structures used to validate the impact damage models.

Item URL in elib:https://elib.dlr.de/67361/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Modelling Damage in Stiffened Composite Panels under High Velocity Impact
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Toso-Pentecote, Nathalienathalie.toso (at) dlr.deUNSPECIFIED
Johnson, Alastairalastair.johnson (at) dlr.deUNSPECIFIED
Date:May 2010
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:IACM
Series Name:IV European Conference on Computational Mechanics
Status:Published
Keywords:composite shell structures, impact damage, FE modelling
Event Title:ECCM 2010: IV European Conference on Computational Mechanics
Event Location:Paris, France
Event Type:international Conference
Event Dates:16-21 May 2010
Organizer:ECCOMAS
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Deposited By: Johnson, Dr.phil. Alastair
Deposited On:09 Jan 2011 18:01
Last Modified:09 Jan 2011 18:01

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