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Simulation of High Velocity Impact on Composite Structures - Model Implementation and Validation

Schueler, Dominik and Toso-Pentecôte, Nathalie and Voggenreiter, Heinz (2016) Simulation of High Velocity Impact on Composite Structures - Model Implementation and Validation. Applied Composite Materials, 23 (4), pp. 857-878. Springer. DOI: 10.1007/s10443-016-9489-0 ISSN 0929-189X

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Official URL: http://link.springer.com/article/10.1007/s10443-016-9489-0

Abstract

High velocity impact on composite aircraft structures leads to the formation of flexural waves that can cause severe damage to the structure. Damage and failure can occur within the plies and/or in the resin rich interface layers between adjacent plies. In the present paper a modelling methodology is documented that captures intra- and inter-laminar damage and their interrelations by use of shell element layers representing sub-laminates that are connected with cohesive interface layers to simulate delamination. This approach allows the simulation of large structures while still capturing the governing damage mechanisms and their interactions. The paper describes numerical algorithms for the implementation of a Ladevèze continuum damage model for the ply and methods to derive input parameters for the cohesive zone model. By comparison with experimental results from gas gun impact tests the potential and limitations of the modelling approach are discussed.

Item URL in elib:https://elib.dlr.de/105511/
Document Type:Article
Title:Simulation of High Velocity Impact on Composite Structures - Model Implementation and Validation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schueler, Dominikdominik.schueler (at) dlr.deUNSPECIFIED
Toso-Pentecôte, NathalieUNSPECIFIEDUNSPECIFIED
Voggenreiter, HeinzUNSPECIFIEDUNSPECIFIED
Date:August 2016
Journal or Publication Title:Applied Composite Materials
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:23
DOI :10.1007/s10443-016-9489-0
Page Range:pp. 857-878
Publisher:Springer
ISSN:0929-189X
Status:Published
Keywords:Composite damage, Delamination, High velocity impact, Non-destructive Evaluation, FE simulation of impact
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures and Materials
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design
Deposited By: Schüler, Dominik
Deposited On:01 Dec 2016 11:11
Last Modified:10 Jan 2019 15:46

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