The Behavior Of Aluminium Carbon/Epoxy Fibre Metal Laminate Under Quasi-Static Loading
One of major concerns that related to the flight safety is impact of birds. To minimize the risks, there is need to increase the impact resistance of aircraft by developing a new material and has the good structural design of aircraft structures. The hybrid laminates are potential candidate material...
| Main Authors: | , , , , , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
IOP Publishing
2017
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| Subjects: | |
| Online Access: | http://umpir.ump.edu.my/id/eprint/19169/ http://umpir.ump.edu.my/id/eprint/19169/ http://umpir.ump.edu.my/id/eprint/19169/ http://umpir.ump.edu.my/id/eprint/19169/1/The%20Behavior%20Of%20Aluminium%20Carbon-Epoxy%20Fibre%20Metal%20Laminate%20Under%20Quasi-Static%20Loading.pdf |