Multiaxial non-crimp fabrics : characterisation of manufacturing capability for composite aircraft primary structure applications
Carbon composite reinforcement fabrics aimed at flight critical aircraft structure application were designed and the capability of the process used to manufacture them examined. Studies of the LIBA multiaxial non-crimp fabric manufacturing process focused on the effect of changes to four manufacturi...
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Cranfield University
1998
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.484667 |