Design and fabrication of an all-composite stabilizer section
In this project, design, development and manufacturing by co-curing of a 3D aerofoil structure was demonstrated by fabricating a typical tapered tail section with two C-spars running through its entire span. The C-spar is bonded at its flange with the skin of the tail section and this forms the main...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2011
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| Online Access: | http://hdl.handle.net/10356/45941 |