Measurements of Mode I Interlaminar Properties of Carbon Fiber Reinforced Polymers Using Digital Image Correlation

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Numerical models based on cohesive zones are usually used to model and simulate the mechanical behavior of laminated carbon fiber reinforced polymers (CFRP) in automotive and aerospace applications and require different interlaminar properties. The current work focuses on determining the interlaminar fracture toughness (GIC) under Mode I loading of a double cantilever beam (DCB) specimen of unidirectional CFRP, serving as prototypical material. The novelty of this investigation is the improvement of the testing methodology by introducing digital image correlation (DIC) as an extensometer and this tool allows for crack growth measurement, phenomenological visualization and quantification of various material responses to Mode I loading. Multiple methodologies from different international standards and other common techniques are compared for the determination of the evolution of GIC as crack resistance curves (R-curves). The primarily metrological sources of uncertainty, in contrast to material specific related uncertainties, are discussed through a simple sensitivity analysis. Additionally, the current work offers a detailed insight into the constraints and assumptions to allow exploration of different methods for the determination of material properties using the DIC measured data. The main aim is an improvement of the measurement technique and an increase in the reliability of measured data during static testing, in advance of future rate dependent testing for crashworthiness simulations.

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652-659

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July 2017

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© 2017 Trans Tech Publications Ltd. All Rights Reserved

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[1] C. Starke, W. Beckert, B. Lauke, Characterization of the delamination behaviour of composites under mode I- and mode II - loading, Materialwiss. Werkstofftech. 27 (1996) 80-89.

DOI: 10.1002/mawe.19960270209

Google Scholar

[2] K. Song, C. G. Dávila, C. A. Rose, Guidelines and parameter selection for the simulation of progressive delamination, Abaqus Users' Conference (2008) 1-15.

Google Scholar

[3] ISO 15024: 2001 (E), Fibre-reinforced plastic composites - Determination of mode I interlaminar fracture toughness, GIC, for unidirectionally reinforced materials, International Standard (2001).

DOI: 10.3403/30448273

Google Scholar

[4] JSA JIS K 7086 ERTA, Testing methods for interlaminar fracture toughness of carbon fibre reinforced plastics, Japanese Industrial Standard, (1997) 1-20.

Google Scholar

[5] EN 6033, DIN EN 6033, Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy - Mode I - GIC, European Standard, (2015).

DOI: 10.3403/30282951

Google Scholar

[6] S. Hashemi, A.J. Kinloch, J.G. Williams, Correction needed in double-cantilever beam tests for assessing the interlaminar failure of fibre composites, J. Mater. Sci. Lett. 8 (1989) 125-129.

DOI: 10.1007/bf00730701

Google Scholar

[7] ASTM D5528-13, Standard test method for mode I interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites, ASTM International, (2013).

DOI: 10.1520/d5528-01r07e01

Google Scholar

[8] A. Beehag, L. Ye., Consolidation and interlaminar fracture properties of unidirectional commingled CF/PEEK composites, J. Thermoplast. Compos. Mater. 9 (1996) 129-150.

DOI: 10.1177/089270579600900203

Google Scholar