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Numerical Simulation of Composite Aircraft Structures under Crash Loading

Kohlgrüber, D. (2000) Numerical Simulation of Composite Aircraft Structures under Crash Loading. In: Proceedings: CEAS Forum on Crash Questions, pp. 77-88. CEAS Forum on Crash Questions, Capua, Italien, 14-15.02.2000.

Full text not available from this repository.

Abstract

The paper describes DLR's research on the crash behaviour of composite energy absorbing structures as used in sub-floor assemblies of modern helicopter and general aviation aircraft. Especially latest developments in the field of numerical simulation of the crash behaviour of these structures using an explicit Finite Element code are presented.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2000,
Title:Numerical Simulation of Composite Aircraft Structures under Crash Loading
Authors:
AuthorsInstitution or Email of Authors
Kohlgrüber, D.UNSPECIFIED
Date:2000
Journal or Publication Title:Proceedings: CEAS Forum on Crash Questions
Page Range:pp. 77-88
Status:Published
Keywords:Numerical simulation, FE code, crash, composite, CFRP, aircraft structures
Event Title:CEAS Forum on Crash Questions, Capua, Italien, 14-15.02.2000
Organizer:AIDAA(Associazione Italiana di Aeronautica ed Astronautica, Naples)
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: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 22:14

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