Lützenburger, M. (2003) CRAHVI D4.3.8 & D 4.4.4a: Simulation results of the A321 DRI-KRASH model including cabin load database. Project Report, DLR-Interner Bericht. 435-2003/20.
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This report presents the results of the simulations which were carried out with a full-scale Airbus A321 DRI-KRASH model for two different crash scenarios. The two selected scenarios are impacts on a rigid surface (with a forward velocity of 70 m/s and a downward velocity of 7 m/s) and 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 input in the CRAHVI cabin load database. Besides accelerations, velocities and displacements which are presented in detail for 5 selected frames, other KRASH simulation results (e.g. energy distribution, wing deformation and loading) are shown. In order to judge the passengers injury risk, a detailed Eiband evaluation was carried out.
|Document Type:||Monograph (Project Report, DLR-Interner Bericht)|
|Title:||CRAHVI D4.3.8 & D 4.4.4a: Simulation results of the A321 DRI-KRASH model including cabin load database|
|Keywords:||simulation, crash, KRASH, global, cabin load|
|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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