Investigation of mechanical behavior of reinforced u-profile composites under low velocity impact

Year 2024, , 218 - 225, 20.12.2024

Merve Uslu , Mete Onur Kaman , Mustafa Albayrak , Cenk Yanen , Serkan Dağ , Serkan Erdem , Kadir Turan

https://doi.org/10.26701/ems.1490393

Abstract

In this study, the impact resistance of reinforced composite panels with unsupported, and U profile supported by I profile was numerically examined. For this purpose, firstly, unsupported glass fiber/epoxy composite panels were designed, and then I-profile composite supports were added to these panels. The impact strength, and damage behavior of supported, and unsupported specimens under low-velocity impact were compared numerically. In the analysis, the MAT22 material card, also known as the Chang-Chang damage model for composite material, was used in the LS-DYNA program. As a result of the analysis, maximum damage load of the unsupported specimen is determined to be approximately 294 N. It was determined that by adding an I profile to the structure, the maximum damage load increased to 543 N. It was seen that the added I profile supports increased the maximum contact force of the composite structure by approximately 85%. Fiber breakage damages were observed in both supported, and unsupported specimens. However, with the use of I profile support, the damaged area was further reduced. It has been determined that under low-velocity impact, supported specimens exhibit more rigid material behavior than unsupported specimens.

Keywords

u-profile composite, Chang-Chang failure criteria, I profile, impact, MAT22.

Ethical Statement

Not applicable

Supporting Institution

This study was supported by Scientific and Technological Research Council of Turkey (TUBITAK) under the Grant Number 123M357

Project Number

123M357

Thanks

Acknowledgments This study was supported by Scientific and Technological Research Council of Turkey (TUBITAK) under the Grant Number 123M357. The authors thank to TUBITAK for their supports.

References

• Hou, Y., Huang, J., Liu, Y., Meng, L., Sapanathan, T., & Xu, Y. (2024). Low-velocity impact and compression after impact behaviors of rib-stiffened CFRP panels: Experimental and numerical study. Aerospace Science and Technology, 146, 108948.
• Hu, C., Xu, Z., Huang, M., Cai, C., Wang, R., & He, X. (2024). An insight into the mechanical behavior and failure mechanisms of T-stiffened composite structures with through-interface debonding defects. Ocean Engineering, 300, 117342.
• Liu, D., Bai, R., Lei, Z., Guo, J., Zou, J., Wu, W., & Yan, C. (2020). Experimental and numerical study on compression-after-impact behavior of composite panels with foam-filled hat-stiffener. Ocean Engineering, 198, 106991.
• Liu, L., & Xu, W. (2022). Effects of fillers on the impact damage and compressive residual properties of single hat-stiffened composite panels. Thin-Walled Structures, 180, 109705.
• Meng, Z., Huang, L., Wang, P., Zhang, W., Sun, J., Zhao, M., Yun, Z., Ai, X., & Li, N. (2024). Investigation on damage behavior of composite T-shaped stiffened panels under compression after multi-point impact considering impact positions. Thin-Walled Structures, 196, 111514.
• Peng, A., Deng, J., Ren, T., Wu, D., Zhou, G., & Wang, X. (2023). On damage behavior and stability of composite T-shaped stiffened panels under compression after impact considering impact locations. Thin-Walled Structures, 182, 110295.
• Shi, G.-J., Xiong, Y., Cai, S.-J., & Wang, D.-Y. (2023). Experiment study of dynamic buckling for stiffened panels under longitudinal impact. Ocean Engineering, 284, 115243.
• Tan, R., Xu, J., Guan, Z., Sun, W., Ouyang, T., & Wang, S. (2020). Experimental study on effect of impact locations on damage formation and compression behavior of stiffened composite panels with L-shaped stiffener. Thin-Walled Structures, 150, 106707.
• Wang, Z., Liu, K., Yu, T., Zong, S., & Wang, X. (2022). Structural deformation mechanism of the hat-stiffened plate used in marine structures under impact load. Ocean Engineering, 266, 112736.
• Wu, X., Chen, Q., Zhao, B., Zhang, K., Wang, P., & Yue, Z. (2022). Experimental behavior and shear bearing capacity simulation of stiffened composite panels subjected to invisible damage impact. Thin-Walled Structures, 178, 109454.
• Zhou, J., Guan, Z., Ouyang, T., Wang, X., Li, Z., & Hu, H. (2022). Experimental investigation of shear fatigue behavior of composite stiffened panels with impact damage. Thin-Walled Structures, 181, 110118.
• Zhou, R., & Gao, W. (2021). Influence of adhesive interface properties on the post-buckling response of composite I-stiffened panels with lateral support under axial compression. Journal of Adhesion Science and Technology, 35(12), 1337–1355.
• Zou, J., Lei, Z., Bai, R., Liu, D., Jiang, H., Liu, J., & Yan, C. (2021). Damage and failure analysis of composite stiffened panels under low-velocity impact and compression after impact. Composite Structures, 262, 113333.
• Li, B., Gong, Y., Gao, Y., Hou, M., & Li, L. (2022). Failure analysis of hat-stringer-stiffened aircraft composite panels under four-point bending loading. Materials, 15(7), 2430.
• Capriotti, M., Kim, H. E., Lanza di Scalea, F., & Kim, H. (2017). Non-Destructive inspection of impact damage in composite aircraft panels by ultrasonic guided waves and statistical processing. Materials, 10(6), 616.
• Albayrak, M., Kaman, M. O., & Bozkurt, I. (2023). Experimental and Numerical Investigation of the Geometrical Effect on Low Velocity Impact Behavior for Curved Composites with a Rubber Interlayer. In Applied Composite Materials (Vol. 30, Issue 2). Springer Netherlands. https://doi.org/10.1007/s10443-022-10094-5
• Berk, B., Karakuzu, R., & Toksoy, A. K. (2017). An experimental and numerical investigation on ballistic performance of advanced composites. Journal of Composite Materials, 51(25), 3467–3480.
• García-Moreno, I., Caminero, M. Á., Rodríguez, G. P., & López-Cela, J. J. (2019). Effect of thermal ageing on the impact damage resistance and tolerance of carbon-fibre-reinforced epoxy laminates. Polymers, 11(1), 160.