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Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle
Öz
This study aims to investigate the low-velocity impact behavior of curved composite plates commonly employed in aviation fuselage and wing surfaces using numerical methods. Layered plates fabricated from E-Glass Epoxy were reinforced with various types of stiffeners and subjected to impacts whit a 12 mm diameter impactor at a velocity of 2.5 m/s. The time-dependent variation of force and displacement on the stiffened curved plates resulting from the impact was analyzed. Furthermore, the temporal variation in the amount of energy absorbed by the plate was observed. The results indicate that plates reinforced with I, T, and blade-type stiffeners absorbed 35.78%, 38.11%, and 37.78% of the impact energy, respectively. Among these, plates with T-type reinforcements exhibited the least post-impact deformation. Particularly noteworthy is the permanent deformation of 3.7 mm experienced by the plate reinforced with blade-type stiffeners.
Anahtar Kelimeler
Teşekkür
This work was conducted scope of Master of Science Thesis of Tolunay Dağ.
Kaynakça
- Adali, S., Cagdas, I. U., Failure analysis of curved composite panels based on first-ply and buckling failures. Procedia Engineering, 10, 1591–1596, 2011.
- Akbulut, M., Sonmez, F. O., Design optimization of laminated composites using a new variant of simulated annealing. Computers and Structures, 89(17–18), 1712–1724, 2011.
- Altin Karataş, M., Gökkaya, H., A review on machinability of carbon fiber reinforced polymer (CFRP) and glass fiber reinforced polymer (GFRP) composite materials. In Defence Technology 14( 4), 318–326, 2018.
- Aytav, E., Işık, A. M., Experimental Investigation of Ballistic Performance of Free Particle Armor Systems. Journal of Materials and Mechatronics: A, 4(2), 518–543, 2023.
- Barkanov, E., Ozoliņš, O., Eglitis, E., Almeida, F., Bowering, M. C., Watson, G., Optimal design of composite lateral wing upper covers. Part I: Linear buckling analysis. Aerospace Science and Technology, 38, 1–8, 2014.
- Correas, A. C., Crespo, A. C., Ghasemnejad, H., Roshan, G., Analytical Solutions to Predict Impact Behaviour of Stringer Stiffened Composite Aircraft Panels. Applied Composite Materials, 28(4), 1237–1254, 2021.
- Dag, T., Yildirim, N., Senturk, G., Durmazoglu, M., Yildirim, S., Uyaner, M., Virtual Investigation on the Response of Glare to Low Velocity Impact. Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, 2023.
- Dağ, T., Yıldırım, N., Kepir, Y., Uyaner, M., E/Cam Epoksi Laminelerin Üzerine Uygulanan Düşük Hızlı Darbe Davranışının Sayısal Simülasyonu. ASREL, 2022.
Ayrıntılar
Birincil Dil
İngilizce
Konular
Kompozit ve Hibrit Malzemeler, Havacılık Malzemeleri, Havacılık Yapıları
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
26 Haziran 2024
Gönderilme Tarihi
27 Mart 2024
Kabul Tarihi
13 Mayıs 2024
Yayımlandığı Sayı
Yıl 2024 Cilt: 5 Sayı: 1
APA
Dağ, T., Güvenç, M. A., & Uyaner, M. (2024). Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle. Journal of Materials and Mechatronics: A, 5(1), 117-129. https://doi.org/10.55546/jmm.1459415
AMA
1.Dağ T, Güvenç MA, Uyaner M. Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle. J. Mater. Mechat. A. 2024;5(1):117-129. doi:10.55546/jmm.1459415
Chicago
Dağ, Tolunay, Mehmet Ali Güvenç, ve Mesut Uyaner. 2024. “Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle”. Journal of Materials and Mechatronics: A 5 (1): 117-29. https://doi.org/10.55546/jmm.1459415.
EndNote
Dağ T, Güvenç MA, Uyaner M (01 Haziran 2024) Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle. Journal of Materials and Mechatronics: A 5 1 117–129.
IEEE
[1]T. Dağ, M. A. Güvenç, ve M. Uyaner, “Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle”, J. Mater. Mechat. A, c. 5, sy 1, ss. 117–129, Haz. 2024, doi: 10.55546/jmm.1459415.
ISNAD
Dağ, Tolunay - Güvenç, Mehmet Ali - Uyaner, Mesut. “Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle”. Journal of Materials and Mechatronics: A 5/1 (01 Haziran 2024): 117-129. https://doi.org/10.55546/jmm.1459415.
JAMA
1.Dağ T, Güvenç MA, Uyaner M. Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle. J. Mater. Mechat. A. 2024;5:117–129.
MLA
Dağ, Tolunay, vd. “Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle”. Journal of Materials and Mechatronics: A, c. 5, sy 1, Haziran 2024, ss. 117-29, doi:10.55546/jmm.1459415.
Vancouver
1.Tolunay Dağ, Mehmet Ali Güvenç, Mesut Uyaner. Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle. J. Mater. Mechat. A. 01 Haziran 2024;5(1):117-29. doi:10.55546/jmm.1459415
Cited By
Low velocity impact response of CFRP and Al2024-T3 helicopter blade
International Journal of Aeronautics and Astronautics
https://doi.org/10.55212/ijaa.1583352