Influence of the Fatigue Load Level and the Hole Diameter on the Laminate Structure’s Fatigue Performance
Damage tolerance of composite aircraft structure is one of the main areas of research, important when a new product is being developed. There are a number of variables, such as damage characteristics (dent depth, delamination area) and loading parameters (load type, amplitude of cyclic loading, load...
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| Format: | Article |
| Language: | English |
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Sciendo
2018-12-01
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| Series: | Fatigue of Aircraft Structures |
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| Online Access: | https://doi.org/10.2478/fas-2018-0002 |