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On damage development in mechanically fastened composite laminates
Royal Inst Technol, Dept Aeronaut, SE-10044 Stockholm, Sweden Saab AB, SE-58188 Linkoping, Sweden.
Royal Inst Technol, Dept Aeronaut, SE-10044 Stockholm, Sweden Saab AB, SE-58188 Linkoping, Sweden.
2000 (English)In: Composite structures, ISSN 0263-8223, E-ISSN 1879-1085, Vol. 49, no 2, 151-171 p.Article in journal (Refereed) Published
Abstract [en]

A comprehensive experimental program was conducted to measure and characterize the development of damage in the vicinity of fastener holes in graphite/epoxy composite laminates. This was carried out to generate data which can be used for development of appropriate failure criteria. Test specimens were loaded in quasi-static cycles with successively increasing loads, and damage development in the vicinity of the bolt holes was detected using different methods such as strain measurements, acoustic emission, X-ray and microscopic examination. Several failure modes were detected in a series of events starting at load levels far below the level at which the first visible evidence of damage appeared on the load-displacement curve. Failure modes included matrix cracking, fibre fracture, delamination and kinking. (C) 2000 Elsevier Science Ltd. All rights reserved.

Place, publisher, year, edition, pages
2000. Vol. 49, no 2, 151-171 p.
Keyword [en]
composite, boltedjoints, failure characterisation, experimental investigation
National Category
Natural Sciences
Identifiers
URN: urn:nbn:se:liu:diva-49789OAI: oai:DiVA.org:liu-49789DiVA: diva2:270685
Available from: 2009-10-11 Created: 2009-10-11 Last updated: 2017-12-12

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