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.

Item URL in elib:

https://elib.dlr.de/15046/

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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Lützenburger, M.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2003

Open Access:

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 (old)

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:

DLR-Beauftragter, elib

Deposited On:

16 Sep 2005

Last Modified:

14 Jan 2010 13:13

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