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MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels

Schueler, Dominik and Toso, Nathalie (2012) MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels. Project Report. DLR-IB 435-2012/22, 46 S.

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Abstract

This part of deliverable D3.5.3 presents a FE methodology to predict impact damage in composite panels using the detailed Ladevèze damage models implemented by DLR. Coupled implicit-explicit techniques are utilized to incorporate static preloads acting in panels subjected to HVI. A discretization method and a material model for ice projectiles are presented for further simulations involving hail impact in Abaqus/Explicit.

Item URL in elib:https://elib.dlr.de/76535/
Document Type:Monograph (Project Report)
Title:MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schueler, Dominikdominik.schueler (at) dlr.deUNSPECIFIED
Toso, Nathalienathalie.toso (at) dlr.deUNSPECIFIED
Date:January 2012
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:46
Keywords:Composites, High Velocity Impact, Preload, Damage, Delamination, Ice Model
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: Schüler, Dominik
Deposited On:23 Jul 2012 12:41
Last Modified:23 Jul 2012 12:41

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