Abstract
Long fiber thermoplastic (LFT) composite/metal laminate (LML) is a hybrid composite consisting of alternate layers of metals such as aluminum and an LFT composite, which combines advantages from both the constituents. The LFT/Al laminates (LMLs) were processed by compression molding and were characterized for their Young’s modulus, mechanical strength, and low-velocity impact (LVI) properties. The average values of specific elastic modulus and specific tensile strength were approximately 20 GPa/(gcm−3) and 108.5 MPa/(gcm−3), respectively. Failure mechanisms included delamination between LFT composite and Al, fiber fracture and pullout in LFT composite, and shear fracture of aluminum and LFT composite layers. Rule-of-mixtures (ROM) predictions of laminate properties in tension compared well with the experimental values. Specific perforation energy of the laminates determined by LVI tests was 7.58 J/(kgm−2), which is significantly greater than that of the LFT composite alone, 1.72 J/(kgm−2). Overall, the LML showed significant improvement in the properties as compared to the LFT composite.
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Acknowledgements
Authors gratefully acknowledge the financial support from Federal Transit Administration (FTA), Contract # W911NF04-2-018. We thank Mr. Pavan Chintalapati for his help with aluminum surface preparation and Dr. Griffin for help in taking SEM pictures.
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Kulkarni, R.R., Chawla, K.K., Vaidya, U.K. et al. Characterization of long fiber thermoplastic/metal laminates. J Mater Sci 43, 4391–4398 (2008). https://doi.org/10.1007/s10853-007-2437-5
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DOI: https://doi.org/10.1007/s10853-007-2437-5