Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/27380
DC FieldValueLanguage
dc.contributorInstitute of Textiles and Clothing-
dc.creatorXiong, J-
dc.creatorZhang, M-
dc.creatorStocchi, A-
dc.creatorHu, H-
dc.creatorMa, L-
dc.creatorWu, L-
dc.creatorZhang, Z-
dc.date.accessioned2015-05-26T08:16:54Z-
dc.date.available2015-05-26T08:16:54Z-
dc.identifier.issn1359-8368-
dc.identifier.urihttp://hdl.handle.net/10397/27380-
dc.language.isoenen_US
dc.publisherPergamon Pressen_US
dc.subjectHoneycomben_US
dc.subjectMechanical propertiesen_US
dc.subjectAnalytical modellingen_US
dc.subjectMechanical testingen_US
dc.titleMechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compressionen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage350-
dc.identifier.epage358-
dc.identifier.volume60-
dc.identifier.doi10.1016/j.compositesb.2013.12.049-
dcterms.abstractMechanical properties and failure modes of carbon fiber composite egg and pyramidal honeycombs cores under in plane compression were studied in the present paper. An interlocking method was developed for both kinds of three-dimensional honeycombs. Euler or core shear macro-buckling, face wrinkling, face inter-cell buckling, core member crushing and face sheet crushing were considered and theoretical relationships for predicting the failure load associated with each mode were presented. Failure mechanism maps were constructed to predict the failure of these composite sandwich panels subjected to in-plane compression. The response of the sandwich panels under axial compression was measured up to failure. The measured peak loads obtained in the experiments showed a good agreement with the analytical predictions. The finite element method was used to investigate the Euler buckling of sandwich beams made with two different honeycomb cores and the comparisons between two kinds of honeycomb cores were conducted.-
dcterms.bibliographicCitationComposites. Part B, Engineering, 2014, v. 60, p. 350-358-
dcterms.isPartOfComposites. Part B, Engineering-
dcterms.issued2014-
dc.identifier.isiWOS:000333506500040-
dc.identifier.scopus2-s2.0-84892754325-
dc.identifier.eissn1879-1069-
dc.identifier.rosgroupidr68401-
dc.description.ros2013-2014 > Academic research: refereed > Publication in refereed journal-
Appears in Collections:Journal/Magazine Article
Access
View full-text via PolyU eLinks SFX Query
Show simple item record

SCOPUSTM   
Citations

37
Last Week
0
Last month
0
Citations as of Sep 6, 2020

WEB OF SCIENCETM
Citations

32
Last Week
0
Last month
0
Citations as of Oct 27, 2020

Page view(s)

140
Last Week
1
Last month
Citations as of Oct 26, 2020

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.