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Modelling Impact Damage in Composite Sandwich Panels

Pentecote, Nathalie and Johnson, Alastair (2005) Modelling Impact Damage in Composite Sandwich Panels. In: EUROPAM 2005 Proceedings CD. EUROPAM 2005, 2005-10-05 - 2005-10-07, Potsdam, Deutschland.

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Abstract

The presentation describes the application of the simulation methods to design studies on a novel form of double-walled composite panels with energy absorbing cores currently being assessed for use in aircraft structures. These are non-standard sandwich structures, in which a main load-bearing composite laminate is protected from impact damage by an energy absorbing core and a second cover laminate. Core materials being considered include folded composite plate structures, polymer foams and Nomex honeycomb. Impact load cases of interest include high velocity impacts from steel impactors and deformable, soft body impactors such as ice. Representative structures are modelled and FE simulation results are presented, which simulate numerically the observed impact failure modes and failure progression under medium to high impact velocities representative of civil aircraft applications.

Item URL in elib:https://elib.dlr.de/20219/
Document Type:Conference or Workshop Item (Speech)
Title:Modelling Impact Damage in Composite Sandwich Panels
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pentecote, NathalieUNSPECIFIEDUNSPECIFIED
Johnson, AlastairUNSPECIFIEDUNSPECIFIED
Date:2005
Journal or Publication Title:EUROPAM 2005 Proceedings CD
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:High Velocity Impact, Composite, sandwich, delamination, High Velocity Impact, Composite, sandwich, delamination
Event Title:EUROPAM 2005
Event Location:Potsdam, Deutschland
Event Type:international Conference
Event Dates:2005-10-05 - 2005-10-07
Organizer:ESI Group
HGF - Research field:Aeronautics, Space and Transport
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: Toso, Dr.-Ing. Nathalie
Deposited On:20 Nov 2006
Last Modified:12 Dec 2013 20:08

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