Bending contact response of composite sandwich beam
The aim of this project is to investigate structural response of honeycomb sandwich beam subjected to bending loads. Face-core delamination is a common un-conventional failure mode of sandwich composites in aerospace structures. Sandwich beam specimens made of unidirectional carbon fibre face (16...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2012
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| Online Access: | http://hdl.handle.net/10356/49362 |