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Review of impact damages modelling in laminated composite aircraft structures

Dragan Kreculj ; University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, 11120 Belgrade, Serbia
Boško Rašuo orcid id orcid.org/0000-0002-0912-6844 ; University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, 11120 Belgrade, Serbia


Puni tekst: hrvatski pdf 1.156 Kb

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Puni tekst: engleski pdf 1.156 Kb

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Sažetak

Laminated composites have an important application in modern aeronautical structures. They have extraordinary properties, like high strength, stiffness and lightweight. Nevertheless, a serious obstacle to more widespread use of those materials is their sensitivity to impact loads. As a consequence of that, impact damage initiation and growth are appearing in them. Failures that occur in laminated composite structures can be intralaminar and interlaminar. To date a lot of models for impact damages in laminates have been developed with higher or lower accuracy. Those models can replace real and expensive testing in laminated structures with some approximation. By using specialized software the damage parameters in laminate aircraft structures can be predicted (at certain conditions). In that way numerical simulation of impact on certain laminates can be done and the obtained results from the simulations presented in a form of graphic damage distributions.

Ključne riječi

damages, impact, laminated composite structures

Hrčak ID:

104076

URI

https://hrcak.srce.hr/104076

Podaci na drugim jezicima: hrvatski

Posjeta: 7.092 *