Title

Vulnerability analysis of aircraft fuselage subjected to internal explosion

Journal title

Archive of Mechanical Engineering

Yearbook

2011

Volume

vol. 58

Issue

No 4

Authors

Dacko, Adam ; Toczyski, Jacek

Keywords

thin-walled structure ; blast wave load ; fluid-structure interaction ; Arbitrary Lagrangian-Eulerian ; ALE ; finite element model ; code LS-Dyna

Divisions of PAS

Nauki Techniczne

Coverage

393-406

Publisher

Polish Academy of Sciences, Committee on Machine Building

Date

2011

Type

Artykuły / Articles

Identifier

DOI: 10.2478/v10180-011-0024-4 ; ISSN 0004-0738, e-ISSN 2300-1895

Source

Archive of Mechanical Engineering; 2011; vol. 58; No 4; 393-406

References

Wentzel C. (2007), Investigation of Vulnerability of Aircraft Structure and Materials Towards Cabin Explosions, null. ; Ashley S. (1992), Safety in the sky: Designing bomb-resistant baggage containers, Mechanical Engineering, 81. ; Moon Y. (1995), Vulnerability and Survivability Analysis of Aircraft Fuselage Subjected to Internal Detonations, null. ; Dacko A. (2010), Structural Response of a Blast Loaded Fuselage, Journal of KONES, 17, 1, 101. ; Habas D. (2008), Selection and Design of Scaled Simplified Sub-Aerostructures. ; Hallquist J. (2010), LS-DYNA V971. ; Soutis C. (2008), Computational Simulation of blast effects on flat panels, null. ; Włodarczyk E. (1994), Wstęp do mechaniki wybuchu [Introduction to Physics of Explosion]. ; Lesuer, D., <i>Failure Modeling of Titanium 6Al-4V and Aluminum 2024-T3 With the Johnson-Cook Material Model</i>, Report FAA: DOT/FAA/AR-03/57, September 2003.