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Integration of Crashworthiness Aspects into Preliminary Aircraft Design

Schwinn, Dominik (2014) Integration of Crashworthiness Aspects into Preliminary Aircraft Design. Applied Mechanics and Materials, 598, pp. 146-150. Trans Tech Publications. DOI: 10.4028/www.scientific.net/AMM.598.146 ISBN 978-3-03835-179-5 ISSN 1660-9336

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Official URL: http://www.scientific.net/AMM.598.146

Abstract

Crashworthiness proof is a certification requirement by aviation authorities for new aircraft types. The objective of static design is a sufficiently stiff and strong structure to carry bending and torsion during flight and ground maneuvers. High stiffness, however, is critical for good crashworthiness behavior. Therefore, crashworthiness investigations should be included at early design stages of the overall aircraft design process. This paper introduces the crash analysis tool AC-CRASH and shows an approach of integrating it into the preliminary design phase.

Item URL in elib:https://elib.dlr.de/90131/
Document Type:Article
Additional Information:Paper was presented on 4th International Conference on Mechanics, Simulation and Control (ICMSC 2014) / 1st International Conference on Aerospace Engineering (ICOAE 2014), June 21-22, 2014, Moscow, Russia
Title:Integration of Crashworthiness Aspects into Preliminary Aircraft Design
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schwinn, Dominikdominik.schwinn (at) dlr.deUNSPECIFIED
Date:16 July 2014
Journal or Publication Title:Applied Mechanics and Materials
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:598
DOI :10.4028/www.scientific.net/AMM.598.146
Page Range:pp. 146-150
Publisher:Trans Tech Publications
Series Name:Advanced Materials, Mechanics and Industrial Engineering
ISSN:1660-9336
ISBN:978-3-03835-179-5
Status:Published
Keywords:Aircraft Crashworthiness; CPACS; Preliminary Design; Parameterization
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures and Materials
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Deposited By: Schwinn, Dominik
Deposited On:20 Aug 2014 11:02
Last Modified:20 Aug 2014 11:02

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