Blast response of metal composite laminate fuselage structures using finite element modelling-Reference-Cited by-同舟云学术

Blast response of metal composite laminate fuselage structures using finite element modelling

Published:2011-01 Issue:2 Volume:93 Page:665-681
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Kotzakolios T.,Vlachos D.E.,Kostopoulos V.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference26 articles.

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3. Moon YI, Bharatram G, Chimmels Capt SA, Venkayya Dr VB. A vulnerability map of a commercial aircraft. In: MSC 1996 world users’ conference proceedings, vol. V; paper no. 44, June 1996.

4. Moon Y, Bharatram G, Schimmels Capt S, Venkayya Dr V. Vulnerability and survivability analysis of aircraft fuselage subjected to internal detonations. In: MSC 1995 world users’ conference proceedings, paper no. 11, May 1995.

5. Pulse pressure loading of aircraft structural panels;Simmons;Thin-Walled Struct,2006

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