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Contribution to an Improved Crash Design for a Composite Transport Aircraft Fuselage - Development of a Kinematics Model and an Experimental Component Test Setup

Waimer, Matthias and Kohlgrüber, Dieter and Keck, Rüdiger and Voggenreiter, Heinz (2013) Contribution to an Improved Crash Design for a Composite Transport Aircraft Fuselage - Development of a Kinematics Model and an Experimental Component Test Setup. CEAS Aeronautical Journal. Springer. DOI: 10.1007/s13272-013-0070-3 ISSN 1869-5590

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Item URL in elib:https://elib.dlr.de/80657/
Document Type:Article
Title:Contribution to an Improved Crash Design for a Composite Transport Aircraft Fuselage - Development of a Kinematics Model and an Experimental Component Test Setup
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Waimer, MatthiasDLR-BKUNSPECIFIED
Kohlgrüber, DieterDLR-BKUNSPECIFIED
Keck, RüdigerDLR-BKUNSPECIFIED
Voggenreiter, HeinzDLR-BKUNSPECIFIED
Date:5 April 2013
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.1007/s13272-013-0070-3
Publisher:Springer
ISSN:1869-5590
Status:Published
Keywords:aircraft crashworthiness, composite transport aircraft fuselage, finite element simulation, frame bending testing, hybrid laminates
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 > Leitungsbereich BK
Institute of Structures and Design > Computer Supported Component Design
Institute of Structures and Design > Structural Integrity
Deposited By: Waimer, Matthias
Deposited On:09 Apr 2013 10:59
Last Modified:08 Mar 2018 19:01

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