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Simulation Methodology for High Velocity Impact in Composite Aircraft Structures

Johnson, A. (2001) Simulation Methodology for High Velocity Impact in Composite Aircraft Structures. In: Air & Space Europe, Vol.3, pp. 56-59. Aeronautics Days, Hamburg, 29-31 Januar 2001.

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Abstract

The paper summarises the IMT Project HICAS on "High Velocity Impact of Composite Aircraft Structures" which was concerned with developing a design methodology and FE simulation tools for predicting the high velocity impact response of composite structures. Achievements include measurement of high rate mechanical properties of three aircraft composite systems, development of new failure models for composites under high rate loads, implementation of models into commercial FE codes and code validation by simulation of impact in test structures.

Item URL in elib:https://elib.dlr.de/14876/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2002, monograph_id=No.3/4,
Title:Simulation Methodology for High Velocity Impact in Composite Aircraft Structures
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Johnson, A.UNSPECIFIEDUNSPECIFIED
Date:2001
Journal or Publication Title:Air & Space Europe
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol.3
Page Range:pp. 56-59
Status:Published
Keywords:design methodology, FE simulation, high velocity impact, aircraft
Event Title:Aeronautics Days, Hamburg, 29-31 Januar 2001
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 22:25

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