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Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle
Abstract
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.
Keywords
Thanks
This work was conducted scope of Master of Science Thesis of Tolunay Dağ.
References
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Details
Primary Language
English
Subjects
Composite and Hybrid Materials, Aerospace Materials, Aerospace Structures
Journal Section
Research Article
Publication Date
June 26, 2024
Submission Date
March 27, 2024
Acceptance Date
May 13, 2024
Published in Issue
Year 2024 Volume: 5 Number: 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, and 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 (June 1, 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, and M. Uyaner, “Low Velocity Impact Behavior of Curved Composite Panels Reinforced with Different Types of Stiffeners Used in Air Vehicle”, J. Mater. Mechat. A, vol. 5, no. 1, pp. 117–129, June 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 (June 1, 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, et al. “Low Velocity Impact Behavior of Curved Composite Panels Reinforced With Different Types of Stiffeners Used in Air Vehicle”. Journal of Materials and Mechatronics: A, vol. 5, no. 1, June 2024, pp. 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. 2024 Jun. 1;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