Influence of interface waviness on delamination characteristics and correlation of through-thickness tensile failure with mode I energy release rates in carbon fibre textile composites

Abstract The delamination initiation and propagation behaviour of layer-wise 3D-textile reinforced carbon fibre/epoxy composites is investigated by through-thickness (TT) tension tests as well as Double Cantilever Beam (DCB) and End-Notch Flexure (ENF) experiments. Different standardised approaches to determine modes I and II strain energy release rates are applied and compared. The results clearly indicate a dependency of the delamination propagation characteristics on the propagation direction, induced by the textile architecture and the according interface waviness. In situ and ex situ computed tomography (CT) is used to investigate TT tensile failure characteristics. The statistical distribution has been investigated considering Gauss and Weibull approaches. A correlation is drawn between the mode I energy release rate derived from the TT testing and traditionally determined values based on DCB testing.

[1]  A. J Brunner,et al.  Experimental aspects of Mode I and Mode II fracture toughness testing of fibre-reinforced polymer-matrix composites , 2000 .

[2]  Clive R. Siviour,et al.  In-plane and through-thickness properties, failure modes, damage and delamination in 3D woven carbon fibre composites subjected to impact loading , 2012 .

[3]  Alastair Johnson,et al.  Computational methods for predicting impact damage in composite structures , 2001 .

[4]  Through-thickness failure of laminated carbon/epoxy composites under combined stress , 1995 .

[5]  Jang-Kyo Kim,et al.  Impact and delamination failure of woven-fabric composites , 2000 .

[6]  Leif A. Carlsson,et al.  The effect of weave pattern and crack propagation direction on mode I delamination resistance of woven glass and carbon composites , 1998 .

[7]  J. H. Kim,et al.  Mechanical properties of woven laminates and felt composites using carbon fibers. Part 2: interlaminar properties , 2004 .

[8]  C. S. Lopes,et al.  Characterization of crack propagation in mode I delamination of multidirectional CFRP laminates , 2012 .

[9]  M. Gude,et al.  A phenomenologically based damage model for 2D and 3D-textile composites with non-crimp reinforcement , 2011 .

[10]  M. Gude,et al.  Determination of strain rate dependent through-thickness tensile properties of textile reinforced thermoplastic composites using L-shaped beam specimens , 2011 .

[11]  C. Cherif,et al.  Thermoplastic composite from innovative flat knitted 3D multi-layer spacer fabric using hybrid yarn and the study of 2D mechanical properties , 2010 .

[12]  T. O'Brien Characterization of delamination onset and growth in a composite laminate , 1982 .

[13]  M. Kotaki,et al.  Effect of interfacial properties and weave structure on mode I interlaminar fracture behaviour of glass satin woven fabric composites , 1997 .

[14]  John C. Brewer,et al.  Quadratic Stress Criterion for Initiation of Delamination , 1988 .

[15]  Sandris Ručevskis,et al.  A Test Device for Damage Characterisation of Composites Based on in Situ Computed Tomography , 2012 .

[16]  The response of a multi-directional composite laminate to through-thickness loading , 2010 .

[17]  Roderick H. Martin,et al.  An Interlaminar Tensile Strength Specimen , 1993 .

[18]  M. I. Jones,et al.  Interlaminar Tensile Strength of Carbon Fibre-Epoxy – Specimen Size, Layup and Manufacturing Effects , 2001 .

[19]  O. Allix,et al.  Interlaminar interface modelling for the prediction of delamination , 1992 .

[20]  Peter Davies,et al.  A status report on delamination resistance testing of polymer-matrix composites , 2008 .

[21]  Michael R Wisnom,et al.  PREDICTION OF DELAMINATION INITIATION AND GROWTH FROM DISCONTINUOUS PLIES USING INTERFACE ELEMENTS , 1998 .

[22]  Andreas J. Brunner,et al.  Mode II fracture testing of composites: a new look at an old problem , 2006 .

[23]  A. Morais,et al.  2960 - MODE I INTERLAMINAR FRACTURE OF CARBON/EPOXY MULTIDIRECTIONAL LAMINATES , 2004 .

[24]  Werner Hufenbach,et al.  The effect of temperature on mechanical properties and failure behaviour of hybrid yarn textile-reinforced thermoplastics , 2011 .

[25]  Wisnom,et al.  Interlaminar Failure of Unidirectional Glass Fibre Epoxy due to Combined Through Thickness Shear and Tension , 1996 .

[26]  Werner Hufenbach,et al.  Polypropylene/glass fibre 3D-textile reinforced composites for automotive applications , 2011 .

[27]  G D Sims,et al.  Understanding limitations of through thickness test methods , 1999 .

[28]  Ian Sinclair,et al.  In situ fibre fracture measurement in carbon-epoxy laminates using high resolution computed tomography , 2011 .

[29]  Werner Hufenbach,et al.  Hybrid 3D-textile reinforced composites with tailored property profiles for crash and impact applications , 2009 .

[30]  Farhad Asgari Mehrabadi Analysis of pure mode III and mixed mode (III + II) interlaminar crack growth in polymeric woven fabrics , 2013 .

[31]  A. Waas,et al.  Resistance to delamination of 3D woven textile composites evaluated using End Notch Flexure (ENF) tests: Experimental results , 2011 .

[32]  Michael R Wisnom,et al.  Size Effects in Interlaminar Tensile and Shear Strength of Unidirectional Glass Fibre/Epoxy , 1996 .

[33]  Robin Olsson,et al.  A survey of test methods for multiaxial and out-of-plane strength of composite laminates , 2011 .