Experimental failure analysis of mechanically fastened joints with clearance in composite laminates under preload
dc.contributor.author | Sen, Faruk | |
dc.contributor.author | Pakdil, Murat | |
dc.contributor.author | Sayman, Onur | |
dc.contributor.author | Benli, Semih | |
dc.date.accessioned | 2024-09-18T20:11:40Z | |
dc.date.available | 2024-09-18T20:11:40Z | |
dc.date.issued | 2008 | |
dc.department | Hatay Mustafa Kemal Üniversitesi | en_US |
dc.description.abstract | A failure investigation was performed to determine the failure mode and bearing strength of mechanically fastened bolted-joints in glass fiber reinforced epoxy laminated composite plates, experimentally. Two different geometrical parameters those are the edge distance-to-hole diameter ratio (E/D) and plate width-to-hole diameter ratio (W/D) were considered. For this purpose, E/D ratio was selected from 1 to 5, whereas W/D ratio was chosen from 2 to 5. Due to determining material parameters effect, laminated plates were stacked as three different group which are [0 degrees/0 degrees/45 degrees/-45 degrees](s), [0 degrees/0 degrees/45 degrees/45 degrees](s) and [0 degrees/0 degrees/30 degrees/30 degrees](s), symmetrically. In addition, the preload moments were applied as 0, 3 and 6 nm, since an important target of this study is to observe the changing of failure mechanism under various preloads. The experiments were also performed under a clearance, for this reason the diameters of the bolt and the circular bolt hole were fixed 5 and 6 mm, respectively. Results showed that failure modes and bearing strengths were considerable affected by the increasing of preloads. Furthermore, when the material and geometrical parameters of composite bolted-joints were changed, the failure behavior and the values of bearing strengths were fully influenced from this changing. (C) 2007 Elsevier Ltd. All rights reserved. | en_US |
dc.identifier.doi | 10.1016/j.matdes.2007.05.009 | |
dc.identifier.endpage | 1169 | en_US |
dc.identifier.issn | 0264-1275 | |
dc.identifier.issn | 1873-4197 | |
dc.identifier.issue | 6 | en_US |
dc.identifier.scopus | 2-s2.0-40849113212 | en_US |
dc.identifier.scopusquality | Q1 | en_US |
dc.identifier.startpage | 1159 | en_US |
dc.identifier.uri | https://doi.org/10.1016/j.matdes.2007.05.009 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12483/9011 | |
dc.identifier.volume | 29 | en_US |
dc.identifier.wos | WOS:000255715800009 | en_US |
dc.identifier.wosquality | Q3 | en_US |
dc.indekslendigikaynak | Web of Science | en_US |
dc.indekslendigikaynak | Scopus | en_US |
dc.language.iso | en | en_US |
dc.publisher | Elsevier Sci Ltd | en_US |
dc.relation.ispartof | Materials & Design | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | composite laminates | en_US |
dc.subject | failure analysis | en_US |
dc.subject | mechanically fastened joints | en_US |
dc.subject | bearing strength | en_US |
dc.subject | bearing mode | en_US |
dc.title | Experimental failure analysis of mechanically fastened joints with clearance in composite laminates under preload | en_US |
dc.type | Article | en_US |
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