Creep response of polymeric honeycombs

Paper


Banerjee, Sourish. 2011. "Creep response of polymeric honeycombs." Bhattacharyya, D., Lin, R. J. T. and Srivatsan, T. S. (ed.) 19th International Symposium on Processing and Fabrication of Advanced Materials (PFAM XIX). Auckland, New Zealand 14 - 17 Jan 2011 Auckland, New Zealand.
Paper/Presentation Title

Creep response of polymeric honeycombs

Presentation TypePaper
Authors
AuthorBanerjee, Sourish
EditorsBhattacharyya, D., Lin, R. J. T. and Srivatsan, T. S.
Journal or Proceedings TitleProceedings of the 19th International Symposium on Processing and Fabrication of Advanced Materials (PFAM XIX)
Number of Pages8
Year2011
Place of PublicationAuckland, New Zealand
ISBN9780473181789
Web Address (URL) of Paperhttp://www.chemie.uni-hamburg.de/tmc/stribeck/pub/PFAM_Zeinolebadi.pdf
Conference/Event19th International Symposium on Processing and Fabrication of Advanced Materials (PFAM XIX)
Event Details
19th International Symposium on Processing and Fabrication of Advanced Materials (PFAM XIX)
Event Date
14 to end of 17 Jan 2011
Event Location
Auckland, New Zealand
Abstract

It is relatively easier to measure experimentally viscoelastic properties of a material. However, when a hollow profile/structure is made of this material, it is not straightforward to predict the viscoelastic response of the cellular structure at the bulk level. This is because of the fact that the cellular material has two different length scales: one at the bulk level and another at the cell level, and hence, the cell level properties significantly affect the bulk behaviour. The aim of this study is to predict the stress relaxation characteristics of the cellular material at the macroscopic level in terms of the stress relaxation characteristics of the cell wall material i.e. at the cell level, topology and cell size. The primary interest is to investigate the out-of-plane viscoelastic properties of the core material. This is because when a sandwich panel is subjected to bending, the core carries primarily the major shear loading in its out-of-plane, whereas the skins carry the major flexural load. Honeycomb made of hexagons (of equal sides) is chosen as topology as it is the most common topology among the cellular cores.

Keywordssandwich panels; hexagons; topology core
ANZSRC Field of Research 2020400510. Structural engineering
400505. Construction materials
401707. Solid mechanics
Byline AffiliationsDepartment of Agricultural, Civil and Environmental Engineering
Institution of OriginUniversity of Southern Queensland
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