TY - JOUR AU - Berrahou, Mohamed AU - Benzineb, Hayet AU - Serier, Mohamed PY - 2022/03/25 Y2 - 2024/03/29 TI - Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack JF - Frattura ed Integrità Strutturale JA - Fra&IntStrut VL - 16 IS - 60 SE - Miscellanea DO - 10.3221/IGF-ESIS.60.23 UR - https://www.fracturae.com/index.php/fis/article/view/3390 SP - 331-345 AB - <p>In this study, the finite element method is used to analyze the effect of corrosion and the behavior of inclined cracks of an aluminum plate Al 2024 -T3 under thermomechanical loading.&nbsp; The effects of the inclination of the crack and the effect of temperature for and different types and shapes of adhesives are highlighted.&nbsp; The results obtained show the increase of the crack inclination leads to a decrease of the damaged area and the damaged area ratio of the adhesive.&nbsp; In addition, the ratio D<sub>R</sub> increases with increasing temperature variation ΔT.&nbsp; The best performing patch shape that gave interesting results during this analysis is the circular and for type the Boron/epoxy is the best.</p> ER -