An experimental and numerical study of the effect of some manufacturing defectsShow others and affiliations
2013 (English)In: ICCM International Conferences on Composite Materials, International Committee on Composite Materials , 2013, p. 4105-4112Conference paper, Published paper (Refereed)
Abstract [en]
During the manufacturing process of composite structural parts, layer of fabrics or unidirectional prepreg may have to be cut in order to fulfil production requirements. From a general mechanical point of view, cutting fibres in a composite part has a large negative impact on the mechanical properties. However, such interventions are necessary in particular cases, for example due to draping of complex geometries. A rather extensive test program was launched to investigate the effects of defects that typically could arise during manufacturing. The overall purpose of the test program was to determine knock-down factors on strength for typical manufacturing defects that occasionally arise and sometimes are hard to avoid in production: cuts/gaps and fibre angle deviations. Four types of specimens were tested, reference, intersection of cuts in adjacent layers combined with a bolt hole, cut in a zero degree ply combined with a bolt hole and specimens with misaligned fibres. The specimens with misaligned fibres were tested with three different fibre angles. In addition to the experimental procedure, FE-analyses utilising cohesive elements were conducted, and after mechanical tests, Non Destructive Investigation (NDI) and fractographic investigations were performed. An excellent correlation between analyses and experiments were obtained.
Place, publisher, year, edition, pages
International Committee on Composite Materials , 2013. p. 4105-4112
Keywords [en]
Experimental, Fractographic investigation, Manufacturing defect, Numerical analysis
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:ri:diva-50040Scopus ID: 2-s2.0-85053216407OAI: oai:DiVA.org:ri-50040DiVA, id: diva2:1478374
Conference
19th International Conference on Composite Materials, ICCM 2013, 28 July 2013 through 2 August 2013
Note
The authors of this paper wishes to express their thanks to the Swedish National Research Programme (NFFP5 Price) who financed the work in this paper. We would also like to thank Tommy Grankäll and Mikael Petersson at Saab Aerostructures for excellent support regarding preparing and manufacturing of specimens used in the experimental procedure of this paper.
2020-10-222020-10-222023-05-08Bibliographically approved