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Effect of thermal aging and fatigue on failure resistance of aerospace composite materials
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.ORCID iD: 0000-0001-9649-8621
2009 (English)In: 5th International EEIGM/AMASE/FORGEMAT Conference on Advanced Materials Research, Bristol: IOP Publishing Ltd , 2009Conference paper, Published paper (Refereed)
Abstract [en]

Exposing a laminate structure to thermal cycles and to temperatures close to the curing temperature, followed by mechanical fatigue, cause interlaminar and intralaminar cracks leading to degradation of the mechanical properties. The effect of thermal and mechanical fatigue, as well as thermal aging, on carbon fiber composite laminate structures is under study in the present paper.

Place, publisher, year, edition, pages
Bristol: IOP Publishing Ltd , 2009.
Series
I O P Conference Series: Materials Science and Engineering, ISSN 1757-8981 ; 5
Keyword [en]
Technology - Chemical engineering
Keyword [sv]
Teknikvetenskap - Kemiteknik
National Category
Composite Science and Engineering
Research subject
Polymeric Composite Materials
Identifiers
URN: urn:nbn:se:ltu:diva-34316DOI: 10.1088/1757-899X/5/1/012020Local ID: 87c89d70-ae72-11de-8293-000ea68e967bOAI: oai:DiVA.org:ltu-34316DiVA: diva2:1007566
Conference
EEIGM/AMASE/FORGEMAT conference on Advanced Materials Research : 04/11/2009 - 05/11/2009
Note
Validerad; 2009; 20091001 (ysko)Available from: 2016-09-30 Created: 2016-09-30 Last updated: 2017-11-25Bibliographically approved

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