Equivalent models of composite corrugated cores with elastomeric coatings for morphing structures

Author:

Dayyani Iman,Friswell Michael I.,Ziaei-Rad Saeed,Saavedra Flores E.I.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference27 articles.

1. Impact behavior and energy absorption of paper honeycomb sandwich panels;Wang;Int J Impact Eng,2005

2. Tipping S, Stojadinovic B, Innovative corrugated steel shear walls for multi-story residential buildings. In: The 14th world conference on earthquake engineering, Beijing, China; 2008.

3. Eifert H, Yu C, Banhart J, Baumeister J, Seeliger W. Weight savings by aluminum metal foams: production, properties and applications in automotive, SAE technical paper 01-0887; 1999. doi: http://dx.doi.org/10.4271/1999-01-0887.

4. McGowan DM, Ambur DR, Damage-tolerance characteristics of composite fuselage sandwich structure with thick face sheets, National aeronautics and space administration, Langley Research Center, Hampton, Virginia; 1997. p. 23681–0001.

5. Heimbs S, Middendorf P, Hampf C, Hähnel F, Wolf K. Aircraft sandwich structures with folded core under impact load. In: Ferreira AJM, editor. 8th International conference on sandwich structures, ICSS 8; 2008.

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