Numerical Analysis Results of Debonding Damage Effects for an SHM System Application on a Typical Composite Beam

Numerical Analysis Results of Debonding Damage Effects for an SHM System Application on a Typical Composite Beam

In the aeronautical field, the damage that occurs to a carbon-fibre-reinforced polymer (CFRP) structure analysis is a crucial point for further improving its capability and performance. In the current the state of the art, in fact, many issues are linked to the certification process more than to tec...

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Bibliografiska uppgifter
Huvudupphovsmän: Gianluca Diodati, Assunta Sorrentino, Lorenzo Pellone, Antonio Concilio, Monica Ciminello, Gianvito Apuleo, Shay Shoham, Iddo Kressel, David Bardenstein
Materialtyp: Artikel
Språk:English
Publicerad: MDPI AG 2023-05-01
Serie:Aerospace
Ämnen:
damage effect
strain modulation
strain sensors
composite structures
bonding lines
FE representation
Länkar:https://www.mdpi.com/2226-4310/10/6/507

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https://www.mdpi.com/2226-4310/10/6/507

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