Toso-Pentecote, Nathalie (2006) CN235-300M Ditching: Behaviour of the Rivets at the Junction Fuselage/Sponson during Ditching impact. DLR-Interner Bericht, Project Report. DLR-IB 435-2006/45.
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This report presents the results of ditching simulations conducted on the forward sponson of the CN235-300M using the explicit finite-element code PAM-CRASH in order to support its ditching certification. The aim is to investigate the response of the rivets at the junction between the fuselage and the forward sponson during ditching basing on test run 25 corresponding to configuration II, which is the likely aircraft ditching configuration. Particularly, rivet failure is of interest.
|Document Type:||Monograph (DLR-Interner Bericht, Project Report)|
|Title:||CN235-300M Ditching: Behaviour of the Rivets at the Junction Fuselage/Sponson during Ditching impact|
|Keywords:||ditching simulation, full-scale aircraft, sponson behaviour|
|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):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Structures and Design > Structural Integrity|
|Deposited By:||Nathalie Toso|
|Deposited On:||28 Dec 2006|
|Last Modified:||27 Apr 2009 13:15|
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