Abstract
Fiber metal laminates (FMLs) are composed of thin metal sheets and fiber-reinforced composite layers. Compared to monolithic aluminum alloys, FMLs combine lower density, higher fatigue resistance, and improved damage tolerance. The present study aimed to investigate the low-velocity impact induced by drop-weight instrument and the tensile strength on various lay-up configurations of FMLs fabricated. FML samples were composed of two layers of aluminum 2024-T3 and two layers of epoxy resin, which were reinforced with carbon fabric, glass fabric, and Kevlar fabric made in pairs. In addition, another type of FMLs was developed with carbon/Kevlar fabric under the same circumstances. Force-time histories of impact forces were recorded, and the damaged specimens were inspected using optical microscopy in terms of the impact side, nonimpact side, and cross-sectional side. Experimental results indicated that the maximum impact force corresponded to the FMLs that were composed of Kevlar fabric on the impact side and glass fabric on the non-impact side. In addition, the highest tensile strength and Young’s modulus among FMLs belonged to FML with Kevlar fabric and glass fabric.
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References
A. Vlot, Report LR-718, Delft University of Technology, Delft, 1993.
R. Eslami-Farsani, S. M. R. Khalili, and V. Daghigh, Int. J. Damage Mech., 23, 729 (2014).
S. Zhu and G. B. Chai, J. Mater. Des. Appl., 228, 301 (2014).
M. Sadighi, R. C. Alderliesten, and R. Benedictus, Int. J. Impact Eng., 49, 77 (2012).
Y. Liu and B. Liaw, Appl Compos. Mater., 17, 43 (2010).
G. R. Villanueva and W. J. Cantwell, Compos. Sci. Technol., 64, 35 (2004).
S. H. Song, Y. S. Byun, T. W. Ku, W. J. Song, J. Kim, and B. S. Kang, J. Mater. Sci. Technol., 26, 327 (2010).
B. Borgonge and M. S. Ypma, Appl. Compos. Mater., 10, 243 (2003).
G. Reyes and H. Kang, J. Mater. Process. Technol., 16, 284 (2007).
A. Vlot, Int. J. Impact Eng., 18, 291 (1996).
ASTM D7136/D7136M-07, “Standard Test Method for Measuring the Damage Resistance of a Fiber-reinforced Polymer Matrix Composite to a Drop-weight Impact Event”, Vol. 15, ASTM Book of Standards, 2005.
G. R. Rajkumar, M. Krishna, H. N. Narasimha Murthy, S. C. Sharma, and K. R. Vishnu Mahesh, Int. J. Soft Comput. Eng., 1, 50 (2012).
ASTM D 3039-00 “Standard Test Methods for Tensile Properties of Polymer Matrix Composite Materials”, Vol. 15, ASTM Book of Standards, 2000.
M. M. Shokrieh, A. Saeedi, and M. Chitsazzadeh, J. Nanostruct. Chem., 3, 1 (2013).
B. M. Liaw, Y. X. Liu, and E. A. Villars, “Proc. of the SEM Annual Conference on Experimental and Applied Mechanics”, USA, 2001.
B. M. Liaw, G. Zeichner, and X. Y. Liu, “Proc. of the SEM International Congress on Experimental Mechanics”, USA, 2000.
A. Vlot, E. Kroon, and G. L. Rocca, Key. Eng. Mater., 141–143, 235 (1998).
E. Sevkat, B. Liaw, and F. Delale, Mater. Des., 52, 67 (2013).
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Sisan, M.M., Eslami-Farsani, R. An Experimental Study on Impact Resistance of Different Layup Configuration of Fiber Metal Laminates. Fibers Polym 20, 2200–2206 (2019). https://doi.org/10.1007/s12221-019-7108-z
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DOI: https://doi.org/10.1007/s12221-019-7108-z