Study on the Effect of Matrix Properties on the Mechanical Performance of Carbon Fabric Composites

Article Preview

Abstract:

Carbon fiber (CF) reinforced compositesusing different types of vinylester (VE)resin includingconventional VE resinhave been prepared. The mechanical performance were characterized by different tests, such as tensile, mode-I interlaminarfracture toughness, tension-tension fatigue and scanning electron microscope (SEM).The experimental results showed that the tensile strength of CF/VE composites changed at a wide range from 22.3% to 37.8% in comparison with the CF/conventional VE composite due to resin type, where the strain at failure was varying. The tensile strength increased with an increase of adhesive strength between carbon fiber and VE resin characterized by the microdroplet test. Namely, a good correlation between the tensile strength of composites and the adhesive strength was found. On the other hand, almost an inverse correlation was found between the tensile strength of composites and the interlaminar fracture toughness of composites obtained by DCB (double cantilever beams) tests. There was no apparent correlation found between the strain at failure for pure resins and the tensile strength of composites.Thefatigue life of CF/VE compositesincreased as well as the tensile strength with an increase of the adhesive strength between carbon fiber and the resin. The samples sometime survived 1000 times longer than that of CF/conventional VE compositewhen the maximum cycle stress was 70% of the tensile strength of the strongest composite.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

38-43

Citation:

Online since:

January 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] W. E. Daniels, ed. Encyclopedia of Polymer Science and Engineering Vol. 17; Wiley: New York, (1985).

Google Scholar

[2] H. Li, A.C. Rosario, S.V. Davis, T. Glass: J. Adv. Mater. Vol 28(1997), p.55.

Google Scholar

[3] P. K. Mallick: FiberReinforcedComposites, Ch. 1. Marcel Dekker, New York (1993).

Google Scholar

[4] N.S. Broyles, K.N.E. Verghese, S.V. Davis, H. Li, R.M. Davis, J.J. Lesko, J.S. Riffle: Polymer Vol. 39(1998), No. 15, p.3417.

DOI: 10.1016/s0032-3861(97)10078-7

Google Scholar

[5] F. Vautard, S. Ozcan, H. Meyer: Composites: Part AVol. 43 (2012), p.1120.

Google Scholar

[6] I.C. Kim, T.H. Yoon:J. Adhesion Sci. Technol. Vol. 14 (2000), No. 4, p.545.

Google Scholar

[7] C.L. Weitzsacker, M. Xie and L. T. Drzal: Surface Interface Anal. Vol. 25(1997), p.53.

Google Scholar

[8] J. Zhu, A. Imam, R. Crane, K. Lozano V.N. Khabashesku, E.V. Barrera: Composites Science and TechnologyVol. 67 (2007), p.1509.

Google Scholar

[9] C. Varga, N. Miskolczi, H. Szakács, G. Lipóczi: Materials and Design Vol. 32(2011), No. 1, p.12.

Google Scholar

[10] P. Compston, P.Y.B. Jar: Appl Compos Mater: Vol. 9(2002), p.291.

Google Scholar

[11] D. Stevanovic,S. Kalyanasundaram, A. Lowe, P.Y.B. Jar: Composites Science and Technology Vol. 63(2003), p. (1949).

Google Scholar

[12] H.Y. Chen, Z.X. Kong, J.H. Wang: Materials Science Forum Vol. 675-677(2011), p.419.

Google Scholar

[13] Y. Liang, R.E. Jensen, D.D. Pappas, G.R. Palmese: PolymerVol. 52(2011), Issue 2, P. 510.

Google Scholar

[14] C.C. Chamis: National Aeronautics and Space Administration Report TN D-5367 (1972).

Google Scholar

[15] P.J. Hine, R.A. Brew, R.A. Duckett, I.M. Ward: Composites Science and Technology Vol. 43(1992), p.37.

Google Scholar

[16] R. Rikards, F.G. Buchhoiz, A.K. Bledzki,G. Wacker, A. Korjakin: Composites Science and Technology Vol. 32 (1996), p.439.

Google Scholar

[17] E.K. Gamstedt, L.A. Berglund, T. Peijs: Composites Science and Technology Vol. 59(1999), p.759.

Google Scholar