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Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures

Kindervater, C.M and Johnson, A, and Kohlgrüber, D, and Lützenburger, M. (2000) Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures. Structural Failure and Plasticity (IMPLAST 2000), IMPLAST 2000, 345-.

Full text not available from this repository.

Abstract

Numerical crash and high velocity simulation studies of metallic and composite sub-components of aircraft structures are presented which were performed within various European Commission (CEC) sponsored research projects. Both hybrid simulation techniques as well as Finite Element (FE) based crash codes were used. Several new composite material models were developed and validated against tests. Especially with the metallic structures, the simulations correlated well with data of impact tests which were performed within the programs.

Item URL in elib:https://elib.dlr.de/14802/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2001,
Title:Crash and High Velocity Impact Simulation Methodologies for Aircraft Structures
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kindervater, C.MUNSPECIFIEDUNSPECIFIED
Johnson, A, UNSPECIFIEDUNSPECIFIED
Kohlgrüber, D, UNSPECIFIEDUNSPECIFIED
Lützenburger, M.UNSPECIFIEDUNSPECIFIED
Date:2000
Journal or Publication Title:Structural Failure and Plasticity (IMPLAST 2000)
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:IMPLAST 2000
Page Range:345-
Status:Published
Keywords:crash, simulation, finite element, numerical analysis, aircraft
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 22:19

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