Adjusting the Flexibility of Fabric Reinforced Composite Laminates Using Experimental Design

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The objective of our work is to improve the mechanical stiffness of fiber reinforced laminates. The stiffness can be characterized by flexural and tensile moduli or their derivation. We applied design of experiments (DOE) to achieve our goals, because to solve the existing analytical and numerical models is complicated.We examined the effects of the following parameters: a) composition of reinforce materials (solely carbon, or carbon and glass combination), b) modulus of resin, c) mass ratio of resin-reinforcement, d) order of layers.The samples manufactured on the basis of DOE were investigated mechanically (flexural and tensile moduli measurements) and morphologically (scanning electron microscopy). We compared the measured modulus results to calculated values.

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181-187

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February 2015

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] David R., The Fundamental Principles of Composite Material Stiffness Predictions, University of the West of England, Bristol, (2006).

Google Scholar

[2] Evgeny V. Morozov, Mechanics and Analysis of Fabric Composites and Structures, AUTEX Research Joumal, Vol. 4 No. 2, South Africa, (2004).

Google Scholar

[3] W. D. Callister, Fundamentals of Materials Science and Engineering, fifth ed., John Wiley and Sons, New York, (2001).

Google Scholar

[4] J. W. Martin, Materials for Engineering, third ed., Woodhead, Cambridge, (2006).

Google Scholar

[5] M. F. Ashby, D. R. H. Jones, Engineering Materials 1, second ed., Butterworth-Heinemann, Oxford, (1996).

Google Scholar

[6] C.S. Verma, V.M. Chariar, Development of layered laminate bamboo composite and their mechanical properties, Composites Part B 43 (2012) 1063-1069.

DOI: 10.1016/j.compositesb.2011.11.065

Google Scholar

[7] C. Dong, I. J. Davies, Flexural and tensile moduli of unidirectional hybrid epoxy composites reinforced by S-2 glass and T700S carbon fibres, Materials and Design 54 (2014) 893-899.

DOI: 10.1016/j.matdes.2013.08.086

Google Scholar

[8] C. Dong, I. J. Davies, Flexural and tensile strengths of unidirectional hybrid epoxy composites reinforced by S-2 glass and T700S carbon fibres, Materials and Design 54 (2014) 955-966.

DOI: 10.1016/j.matdes.2013.08.087

Google Scholar

[9] H. He, J. Wangb, K. Li, J. Wanga, J. Gu Mixed resin and carbon fibres surface treatment for preparation of carbon fibres composites with good interfacial bonding strength, Materials and Design 31 (2010) 4631-4637.

DOI: 10.1016/j.matdes.2010.05.031

Google Scholar

[10] R. Rikards, A. Chate, Identification of Elastic Properties of Composites by Method of Planning of Experiments, Composite Structures 42 (1998) 257-263.

DOI: 10.1016/s0263-8223(98)00071-3

Google Scholar

[11] R. Rikards, A. Chate, G. Gailis, Identification of Elastic Properties of Laminates Based on Experiment Design, International Journal of Solids and Structures 38 (2001) 5097-5115.

DOI: 10.1016/s0020-7683(00)00349-8

Google Scholar

[12] R. Rikards, A. Chate, W. Steinchen, A. Kessler, A.K. Bledzki, Method for identification of elastic properties of laminates based on experiment design, Composites Part B 30 (1999) 279–289.

DOI: 10.1016/s1359-8368(98)00059-6

Google Scholar