On the determination of delamination toughness by using multidirectional DCB specimens
In: Polymer testing, Jg. 29 (2010), Heft 6, S. 658-666
Online
academicJournal
- print, 23 ref
Zugriff:
This work covers the problems encountered in correctly determining mode I interlaminar fracture toughness of composite materials. Pure mode I tests were performed on double cantilever beam (DCB) specimens composed by quasi-homogeneous and uncoupled multidirectional (MD) laminates using 16 or 26-ply: [α/-α2/α/-α/α2/-α]symoranti-sym and [O/α/-α/O2/-α/O/α/O2/α/-α/O]sym, with a = O°,15°,30°,45°,90°. A finite element analysis shows that the non-uniformity ratio β=(GImax-GIav.)/GIav% depends not only on the parameter Dc = D212/(D11D22), but also on the specimen geometrical ratios a/b and a/h. The condition of Dc<0.25 is not sufficient to assure a uniform GI width-wise distribution. If we want to study the crack growth between any ply angles, it is difficult to find lay-ups having β<10%. In fact, the crack initiation in MD DCB specimens usually occurred at the middle of the specimens, where GI attained a maximum. Hence, the critical energy release rate GIC has to be measured by the maximum instead of the mean of Gi.
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On the determination of delamination toughness by using multidirectional DCB specimens
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Autor/in / Beteiligte Person: | GONG, X. J ; HUREZ, A ; VERCHERY, G |
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Zeitschrift: | Polymer testing, Jg. 29 (2010), Heft 6, S. 658-666 |
Veröffentlichung: | Kindlington: Elsevier, 2010 |
Medientyp: | academicJournal |
Umfang: | print, 23 ref |
ISSN: | 0142-9418 (print) |
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