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CRAHVI D 4.3.6: Simulation results of the A380 DRI-KRASH model due to slope impact including cabin load database

Lützenburger, M. (2003) CRAHVI D 4.3.6: Simulation results of the A380 DRI-KRASH model due to slope impact including cabin load database. Project Report, DLR-Interner Bericht. 435-2003/28.

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Abstract

This report presents the results of the simulations which were carried out with a full-scale Airbus A380 DRI-KRASH stick model for a slope impact scenario (on a 10° slope with a forward velocity of 60 m/s and a downward velocity of 4 m/s). These simulations are a DLR contribution to CRAHVI Tasks 4.3 and 4.4 where the generated results are entered in the CRAHVI cabin load database. Accelerations and displacements which are input in the load database are presented in detail for 5 selected fuselage sections. Additionally, other global KRASH simulation results (e.g. energy distribution, wing deformation and loading) are also shown in this report.

Document Type:Monograph (Project Report, DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2004,
Title:CRAHVI D 4.3.6: Simulation results of the A380 DRI-KRASH model due to slope impact including cabin load database
Authors:
AuthorsInstitution or Email of Authors
Lützenburger, M.UNSPECIFIED
Date:2003
Status:Published
Keywords:simulation, global, KRASH, model, slope impact
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
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 13:13

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