File Download
  Links for fulltext
     (May Require Subscription)
Supplementary

Article: A semi-analytical method for bending, buckling, and free vibration analyses of sandwich panels with square-honeycomb cores

TitleA semi-analytical method for bending, buckling, and free vibration analyses of sandwich panels with square-honeycomb cores
Authors
KeywordsBending
Free vibration
Global buckling
Hamilton's principle
Sandwich panels with square-honeycomb cores
Issue Date2010
PublisherWorld Scientific Publishing Co Pte Ltd. The Journal's web site is located at http://www.worldscinet.com/ijssd/ijssd.shtml
Citation
International Journal Of Structural Stability And Dynamics, 2010, v. 10 n. 1, p. 127-151 How to Cite?
AbstractA semi-analytical method for bending, global buckling, and free vibration analyses of sandwich panels with square-honeycomb cores is presented. The discrete geometric nature of the square-honeycomb core is taken into account by treating the core sheets as thin beams and the sandwich panel as composite structure of plates and beams with proper displacement compatibility. Based on the classical model of sandwich panels, the governing equations of motion of the discrete structure are derived using Hamilton's principle. Closed-form solutions are developed for bending, global buckling, and free vibration of simply supported square-honeycomb sandwich panels by employing Fourier series and the Galerkin approach. Results from the proposed method agree well with available results in the literature and those from detailed finite element analysis. The effects of various geometric parameters of the sandwich panel on its behavior are investigated. The present method provides an efficient way of analysis and optimization of sandwich panels with square-honeycomb cores. © 2010 World Scientific Publishing Company.
Persistent Identifierhttp://hdl.handle.net/10722/124607
ISSN
2015 Impact Factor: 1.028
2015 SCImago Journal Rankings: 0.613
ISI Accession Number ID
References

 

DC FieldValueLanguage
dc.contributor.authorLiu, Jen_HK
dc.contributor.authorCheng, YSen_HK
dc.contributor.authorLi, RFen_HK
dc.contributor.authorAu, FTKen_HK
dc.date.accessioned2010-10-31T10:43:53Z-
dc.date.available2010-10-31T10:43:53Z-
dc.date.issued2010en_HK
dc.identifier.citationInternational Journal Of Structural Stability And Dynamics, 2010, v. 10 n. 1, p. 127-151en_HK
dc.identifier.issn0219-4554en_HK
dc.identifier.urihttp://hdl.handle.net/10722/124607-
dc.description.abstractA semi-analytical method for bending, global buckling, and free vibration analyses of sandwich panels with square-honeycomb cores is presented. The discrete geometric nature of the square-honeycomb core is taken into account by treating the core sheets as thin beams and the sandwich panel as composite structure of plates and beams with proper displacement compatibility. Based on the classical model of sandwich panels, the governing equations of motion of the discrete structure are derived using Hamilton's principle. Closed-form solutions are developed for bending, global buckling, and free vibration of simply supported square-honeycomb sandwich panels by employing Fourier series and the Galerkin approach. Results from the proposed method agree well with available results in the literature and those from detailed finite element analysis. The effects of various geometric parameters of the sandwich panel on its behavior are investigated. The present method provides an efficient way of analysis and optimization of sandwich panels with square-honeycomb cores. © 2010 World Scientific Publishing Company.en_HK
dc.languageengen_HK
dc.publisherWorld Scientific Publishing Co Pte Ltd. The Journal's web site is located at http://www.worldscinet.com/ijssd/ijssd.shtmlen_HK
dc.relation.ispartofInternational Journal of Structural Stability and Dynamicsen_HK
dc.rightsCreative Commons: Attribution 3.0 Hong Kong License-
dc.rightsElectronic version of an article published as International Journal of Structural Stability and Dynamics, 2010, v. 10 n. 1, p. 127-151 [http://dx.doi.org/10.1142/S0219455410003361] © World Scientific Publishing Company. http://www.worldscinet.com/ijssd/ijssd.shtml-
dc.subjectBendingen_HK
dc.subjectFree vibrationen_HK
dc.subjectGlobal bucklingen_HK
dc.subjectHamilton's principleen_HK
dc.subjectSandwich panels with square-honeycomb coresen_HK
dc.titleA semi-analytical method for bending, buckling, and free vibration analyses of sandwich panels with square-honeycomb coresen_HK
dc.typeArticleen_HK
dc.identifier.openurlhttp://library.hku.hk:4550/resserv?sid=HKU:IR&issn=0219-4554&volume=10&issue=1&spage=127&epage=151&date=2010&atitle=A+semi-analytical+method+for+bending,+buckling,+and+free+vibration+analyses+of+sandwich+panels+with+square-honeycomb+coresen_HK
dc.identifier.emailAu, FTK:francis.au@hku.hken_HK
dc.identifier.authorityAu, FTK=rp00083en_HK
dc.description.naturepostprint-
dc.identifier.doi10.1142/S0219455410003361en_HK
dc.identifier.scopuseid_2-s2.0-77951527449en_HK
dc.identifier.hkuros175832en_HK
dc.relation.referenceshttp://www.scopus.com/mlt/select.url?eid=2-s2.0-77951527449&selection=ref&src=s&origin=recordpageen_HK
dc.identifier.volume10en_HK
dc.identifier.issue1en_HK
dc.identifier.spage127en_HK
dc.identifier.epage151en_HK
dc.identifier.isiWOS:000275713800008-
dc.publisher.placeSingaporeen_HK
dc.identifier.scopusauthoridLiu, J=36071188200en_HK
dc.identifier.scopusauthoridCheng, YS=7404911293en_HK
dc.identifier.scopusauthoridLi, RF=35173172000en_HK
dc.identifier.scopusauthoridAu, FTK=7005204072en_HK

Export via OAI-PMH Interface in XML Formats


OR


Export to Other Non-XML Formats