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5. Conclusion
This article presents examples and case studies of thermomechanical, diffusive-mechanical and thermochemical-mechanical-oxidative couplings that occur during the ageing of organic matrix composites for aeronautical and aerospace applications. For each type of coupling, the steps of experimental characterization, modeling, identification and simulation have been addressed, based on existing bibliographical references and, in part, on research work conducted by the authors.
It should be emphasized that all the aspects reviewed in this article are not exhaustive, as other types of ageing can take place (radiochemical ageing, ageing by irradiation, ablation, exposure to fire, etc.). Further information on these types of aging in polymer materials can be found in the references
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Conclusion
Bibliography
Events
DURACOSYS – DURAbility of Composite SYStems – International conference series on the durability of composite materials and systems.
ICCM – International Conference on Composite Materials – International conference series on composite materials.
ECCM – European Conference on Composite Materials – International conference series on composite materials.
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Standards and norms
Durability standards for composite materials
- Federal aviation regulations – Part 25: material strength properties and design values - FAR 25.613 - 2003
- Federal aviation administration – Advisory circular – Composite aircraft structure - FAA AC 20-107A - 2009
- Federal aviation regulations – Part 25: Materials - FAR 25.603 - 1978
- Federal aviation regulations – Part 25: Fabrication methods...
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Federal Aviation Administration (FAA) – Government agency responsible for regulations and controls concerning civil aviation in the United States.
Joint Aviation Authorities (JAA) – Organization associated with the ECAC (European Civil Aviation Conference) in the harmonization of civil aviation in Europe. Since 2009, it has been...
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