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: | Michael May, Sonja Arnold-Keifer, Thomas Haase |
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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 |
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