Damage resistance of composite structures with unsymmetrical stacking sequence subjected to high velocity bird impact
It is current aerospace standard to design composite laminates using a zero [B]-matrix in order to avoid warpage during manufacturing. A zero [B]-matrix is typical for symmetric laminates, thus making symmetric stacking sequences the preferred choice in aerospace designs. In recent works, unsymmetri...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2020-08-01
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| Series: | Composites Part C: Open Access |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2666682020300025 |