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Modelling the postbuckling behaviour of impacted composite aerostructures
Imperial College London.
Monash University.
RISE, Swerea, Swerea SICOMP.
2009 (English)In: ICCM International Conferences on Composite MaterialsConference paper, Published paper (Refereed)
Abstract [en]

Two approaches to modelling the effects of embedded defects and impact damage in composite aerostructures are presented. These differ in the manner n which the damage is represented; one as an equivalent delamination and the other as a soft inclusion with non-linear homogenized material properties. These techniques are applied to study the effects of defects and impact damage on the performance of composite panels.

Place, publisher, year, edition, pages
2009.
Keyword [en]
Delamination, Impact damage, Postbuckling, Soft inclusion, Stiffened panel
National Category
Materials Engineering
Identifiers
URN: urn:nbn:se:ri:diva-13119Scopus ID: 2-s2.0-80052039638OAI: oai:DiVA.org:ri-13119DiVA: diva2:973315
Conference
17th International Conference on Composite Materials, ICCM-17
Available from: 2016-09-22 Created: 2016-09-22Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
  • ieee
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  • vancouver
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