Experimental Investigation of CFRP Impact Toughness and Failure Modes

Authors

  • Ondřej Flášar University of Defence in Brno, Czech Republic

DOI:

https://doi.org/10.3849/aimt.01214

Keywords:

composite, impact, pendulum, impact toughness, bending, failure mode

Abstract

The experimental investigation assesses the capability of Carbon Fibre Reinforced Plastics (CFRP) to absorb impact energy. The method is based on measuring impact toughness of unnotched beam specimens made of laminates with woven and unidirectional reinforcement in either cross‐ply [0/90]n or angle‐ply [±45]n orientation using impact pendulum testing machine. Low‐velocity impact produces interlaminar and intralaminar failures of beams which affect their energy absorptions. The resulting energy absorptions are evaluated from force‐displacement curves and subsequently discussed using assessment of loading processes and final failure modes.

Author Biography

  • Ondřej Flášar, University of Defence in Brno, Czech Republic

    Ph.D. candidate on Department of Airforce and Aircraft Technologies, Faculty of Military Technology, University of Defence in Brno

References

GRADY, J. Fracture Toughness Testing of Polymer Matrix Composites [Technical report]. NASA‐TP-3199, USA, 1992.

NIU M.C.Y. Composite Airframe Structures. Hong Kong: Conmilit, 1992.

ASTM D6110-10, Standard Test Method for Determining the Charpy Impact Resistance of Notched Specimens of Plastics. ASTM International, 2010.

ASTM E2248-15, Standard Test Method for Impact Testing of Miniaturized Charpy V-Notch Specimens. ASTM International, 2015.

CAMINERO, M.A., RODRÍGUEZ, G.P. and MUÑOZ, V. Effect of Stacking Sequence on Charpy Impact and Flexural Damage Behavior of Composite Laminates. Composite Structures, 2016, vol. 136, p. 345-357. ISSN 0263-8223. https://doi.org/10.1016/j.compstruct.2015.10.019.

KIM, K.W. et al. Cure Behaviors and Mechanical Properties of Carbon Fiberreinforced Nylon6/epoxy Blended Matrix Composites. Composites Part B: Engineering, 2017, vol. 112, p. 15-21. ISSN 1359-8368. https://doi.org/10.1016/j.compositesb.2016.12.009.

AHMED, K.S., MALLINATHA, V. and AMITH, S.J. Effect of Ceramic Fillers on Mechanical Properties of Woven Jute Fabric Reinforced Epoxy Composites.Journal of Reinforced Plastics and Composites, 2011, vol. 30, no. 15, p. 1315-1326. ISSN 0731-6844. https://doi.org/10.1177/0731684411420606.

HASANI, H., AJELI, S., HESSAMI, R. and ZADHOUSH, A. Investigation into Energy Absorption Capacity of Composites Reinforced by Three-dimensionalweft Knitted Fabrics. Journal of Industrial Textiles, 2014, vol. 43, no. 4, p. 536-548. ISSN 1528-0837. https://doi.org/10.1177/1528083712468604.

KAVITHA, N., BALASUBRAMANIAN, M. and KENNEDY, A.X. Investigation of Impact Behavior of Epoxy Reinforced with Nanometer- and micrometersized Silicon Carbide Particles. Journal of Composite Materials, 2013, vol. 47, no. 15, p. 1877-1884. ISSN 0021-9983. https://doi.org/10.1177/0021998312451920.

ASOPA, V. et al. A Comparative Evaluation of Properties of Zirconia Reinforced High Impact Acrylic Resin with that of High Impact Acrylic Resin. The Saudi Journal for Dental Research, 2015, vol. 6, no. 2, p. 146-151. ISSN 2352-0035. https://doi.org/10.1016/j.sjdr.2015.02.003.

ASTM D256-10e1, Standard Test Methods for Determining the Izod Pendulum Impact Resistance of Plastics. ASTM International, 2010.

WEISBROD, G. and RITTEL, D. A Method for Dynamic Fracture Toughness Determination using Short Beams. International Journal of Fracture, 2000, vol. 104, no. 1, p. 89-103. ISSN 0376-9429. https://doi.org/10.1023/A:1007673528573.

DE CICCO, D., ASAEE, Z. and TAHERI, F. Low-velocity Impact Damage Response of Fiberglass / Magnesium Fiber-metal Laminates under Different Size and Shape Impactors. Mechanics of Advanced Materials and Structures, 2017, vol. 24, no. 2, p. 545-555. ISSN 1537-6494. https://doi.org/10.1080/15376494.2016.1162343.

XU, W. and WAAS, A.M. Fracture Toughness of Woven Textile Composites. Engineering Fracture Mechanics, 2017, vol. 169, p. 184-188. ISSN 0013-7944. https://doi.org/10.1016/j.engfracmech.2016.11.027.

HARRIS, B. Engineering Composite Materials. London: Institute of Metals, 1999.

TRONSKAR, J.P., MANNAN, M.A. and LAI, M.O. Measurement of Fracture Initiation Toughness and Crack Resistance in Instrumented Charpy Impact Testing. Engineering Fracture Mechanics, 2002, vol. 69, no. 3, p. 321-338. ISSN 0013-7944. https://doi.org/10.1016/S0013-7944(01)00077-7.

HART, K.R. and WETZEL, E.D. Fracture Behavior of Additively Manufactured Acrylonitrile Butadiene Styrene (ABS) Materials. Engineering Fracture Mechanics, 2017, vol. 177, p. 1-13. ISSN 0013-7944. https://doi.org/10.1016/j.engfracmech.2017.03.028.

HARRIS, B. Micromechanisms of Crack Extension in Composites. Metal Science, 1980, vol. 14, no. 8-9, p. 351-362. ISSN 0306-3453. https://doi.org/10.1179/msc.1980.14.8-9.351.

TOMITA, Y. and MORIOKA. K. Effect of Lay-up Sequence on Mechanical Properties and Fracture Behaviour of Advanced CFRP Laminate Composite. Materials Science and Engineering: A, 1997, vol. 234-236, p. 778-781. ISSN 0921-5093. https://doi.org/10.1016/S0921-5093(97)00411-5.

MORIOKA, K. and TOMITA, Y. Effect of Lay-up Sequence on Mechanical Properties and Fracture Behaviour of CFRP Laminate Composites. Materials Characterization, 2000, vol. 45, no. 2, p. 125-136. ISSN 1044-5803. https://doi.org/10.1016/S1044-5803(00)00065-6.

RICHARDSON, M.O.W. and WISHEART, M.J. Review of Low-velocity Impact Properties of Composite Materials. Composites Part A: Applied Science and Manufacturing, 1996, vol. 27, no. 12, p. 1123-1131. ISSN 1359-835X. https://doi.org/10.1016/1359-835X(96)00074-7.

TARPANI, J.R., MALUF, O. and GATTI, M.C.A. Charpy Impact Toughness of Conventional and Advanced Composite Laminates for Aircraft Construction. Materials Research, 2009, vol. 12, no. 4, p. 395-403. ISSN 1516-1439. https://doi.org/10.1590/S1516-14392009000400004.

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Published

23-05-2018

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Research Paper

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How to Cite

Flášar, O. (2018). Experimental Investigation of CFRP Impact Toughness and Failure Modes. Advances in Military Technology, 13(1), 47-58. https://doi.org/10.3849/aimt.01214