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Evaluation of material properties and internal damage within CFRP and CFRP/Al sandwich panels due to impact loading

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Abstract

In the present paper, damage development within Carbon fiber reinforced plastic (CFRP) laminates and CFRP/Aluminum (Al) honeycomb core sandwich panels by impact loading was evaluated, and change in material properties due to the damage development was investigated. Falling weight impact tests, 3-point bending tests and cross-sectional observation were carried out. As results, it is found that falling rate of bending elastic modulus due to internal damage in the laminate only is lower than that in the upper face-sheet of the sandwich panel, and that difference in the falling rate between them becomes maximum at the impact energy of 5.1 J. As a result of investigating the relationship between reduction in bending elastic modulus and internal damage development, the reduction is caused by delamination within CFRP laminates mainly. Since total length of cracks in CFRP/Al honeycomb core sandwich panels is smaller than that in the laminates only, the sandwich panels have high impact tolerance because of absorption of impact energy by damaging Al honeycomb core.

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References

  1. K. Tanaka, T. Kurokawa, S. Fujinaga and M. Katou, Damage and residual bending strength of graphite/epoxy composite laminates subjected to nomal impact, Aeronautical and Space Sciences Japan, 37 (425) (1989) 285–292.

    Article  Google Scholar 

  2. K. Fujii, M. Aoki, N. Kiuchi, E. Yasuda and Y. Tanabe, Impact perforation behavior of CFRPs using high-velocity steel sphere, International Journal of Impact Engineering, 27 (2002) 497–508.

    Article  Google Scholar 

  3. B. Wang, G. Zhang, S. Wang, L. Ma and L. Wu, High velocity impact response of composite lattice core sandwich structures, Applied Composite Materials, 21 (2) (2014) 377–389.

    Article  Google Scholar 

  4. M. Salvetti, A. Gilioli, C. Sbarufatti, K. Dragan, M. Chalimoniuk, A. Manes and M. Giglio, Analytical model to describe damage in CFRP specimen when subjected to low velocity impacts, Procedia Engineering, 167 (2016) 2–9.

    Article  Google Scholar 

  5. J. Zhang, L. Zhao, M. Li and Y. Chen, Compressive fatigue behavior of low velocity impacted and quasi-static indented CFRP laminates, Composites Structures, 133 (2015) 1009–1015.

    Article  Google Scholar 

  6. Md. A. Hazizan and W. J. Cantwell, The low velocity impact response of foam-based sandwich structures, Composites: Part B, 33 (2002) 193–204.

    Article  Google Scholar 

  7. J. P. Charles and D. Guedra-Degeorges, Impact damage tolerance of helicopter sandwich structures, Proc. 23rd Int. SAMPE Conf., Kiamesha Lake, NY, USA (1991) 51–61.

    Google Scholar 

  8. M. D. Rhodes, Impact fracture of composite sandwich structures, Proc. ASME/AIAA/SAE, 16th Struct., Struct. Dyn. Mat. Conf., Denver, CO, USA (1975) 311–316.

    Google Scholar 

  9. Y. Chen, S. Hou, K. Fu, X. Han and L. Ye, Low-velocity impact response of composite sandwich structures: Modelling and experiment, Composite Structures, 168 (2017) 322–334.

    Article  Google Scholar 

  10. I. M. Daniel, J. L. Abot, P. M. Schubel and J.-J. Luo, Response and damage tolerance of composite sandwich structures under low velocity impact, Experimental Mechanics, 52 (2012) 37–47.

    Article  Google Scholar 

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Correspondence to Mamoru Mizuno.

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Masahiro Hosoi is a master course student at Graduate School of Akita Prefectural University in Yurihonjo, Akita, Japan. His current research interests include evaluation of internal damage within CFRP due to impact loading and the effect of the damage on material properties of CFRP.

Mamoru Mizuno received his Dr. degree in Engineering from Nagoya University in Nagoya, Aichi, Japan. He is a Professor at Department of Machine Intelligence and Systems Engineering, Akita Prefectural University. His main subjects are evaluation of internal damage within engineering materials, modeling of the damage and numerical simulation of deformation in engineering materials including the damage.

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Hosoi, M., Mizuno, M. & Shi, J. Evaluation of material properties and internal damage within CFRP and CFRP/Al sandwich panels due to impact loading. J Mech Sci Technol 31, 4079–4084 (2017). https://doi.org/10.1007/s12206-017-0803-z

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  • DOI: https://doi.org/10.1007/s12206-017-0803-z

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