Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
The increasing demand for greener aviation technology has driven the adoption of advanced composite materials in aircraft structures, offering significant weight saving and fuel efficiency improvements. Wing structures made of torsion boxes composed of stiffened panels have shown over the decades th...
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| Автори: | , , , , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
Sciendo
2025-07-01
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| Серія: | Fatigue of Aircraft Structures |
| Предмети: | |
| Онлайн доступ: | https://doi.org/10.2478/fas-2024-0004 |
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