Mechanical behavior of flat and curved laminates interleaved by electrospun nanofibers
A major weakness of composite materials is that low-velocity impact, introduced accidentally during manufacture, operation or maintenance of the aircraft, may result in delaminations between the plies. Therefore, the first part of this study is focused on mechanics of curved laminates...
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| Format: | Doctoral Thesis |
| Language: | en |
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Alma Mater Studiorum - Università di Bologna
2014
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| Online Access: | http://amsdottorato.unibo.it/6598/ |