The impact behaviour of carbon fiber-epoxy composite leading edge using finite element method
Composite material has been widely used in aircrafts due to its high strength to weight ratio that leads to weight saving of the aircrafts. Equally important, aircraft material should be tough i.e. it should have the ability to absorb high energy and thus resist fracture. The aircraft's wing de...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Blue Eyes Intelligence Engineering and Sciences Publication,
2019-07.
|
| Subjects: | |
| Online Access: | Get fulltext |