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