Improving the open-hole tension characteristics with variable-axial composite laminates: Optimization, progressive damage modeling and experimental observations

Abstract This study consists of a numerical and experimental investigation on unnotched and open-hole tensile characteristics of fiber-steered variable-axial (also known as variable angle-tow and variable-stiffness) composite laminates. The fiber path was obtained from an optimization framework considering manufacturing characteristics of the Tailored Fiber Placement (TFP) process, in which both fiber angle and thickness are locally optimized; besides, unnotched coupons, open-hole samples with unidirectional fibers, fibers along principal stress directions and with optimized fiber path were manufactured and tested under longitudinal tensile loading. The tests were assisted by digital image correlation (DIC) to accurately capture both strain field and failure behavior. A progressive damage model was then developed to simulate the experimental observations. The notched strength-to-weight of the open-hole coupon with an optimized fiber pattern has a notched strength even higher than the unnotched sample. Optical measurements via DIC and numerical predictions evidenced no strain concentrations around the hole near the final failure for coupons with optimized fiber path, where the reinforcing mechanism alleviated the strain concentrations by redistributing the stress uniformly around the coupon.

[1]  José Humberto S. Almeida,et al.  Carbon fiber-reinforced epoxy filament-wound composite laminates exposed to hygrothermal conditioning , 2016, Journal of Materials Science.

[2]  K. Gliesche,et al.  Application of the tailored fibre placement (TFP) process for a local reinforcement on an “open-hole” tension plate from carbon/epoxy laminates , 2003 .

[3]  Lincy Pyl,et al.  Exploration of the design freedom of 3D printed continuous fibre-reinforced polymers in open-hole tensile strength tests , 2019, Composites Science and Technology.

[4]  Seng C. Tan,et al.  A Progressive Failure Model for Composite Laminates Containing Openings , 1991 .

[5]  Paul M. Weaver,et al.  Computer aided modelling of variable angle tow composites manufactured by continuous tow shearing , 2015 .

[6]  Don Kelly,et al.  On the design, manufacture and testing of trajectorial fibre steering for carbon fibre composite laminates☆ , 2000 .

[7]  Shijie Qi,et al.  Variable Angle Tow reinforcement design for locally reinforcing an open-hole composite plate , 2018, Composite Structures.

[8]  Notched response of non-crimp fabric thin-ply laminates: Analysis methods , 2013 .

[9]  Jerzy Warminski,et al.  A review on the mechanical behaviour of curvilinear fibre composite laminated panels , 2014 .

[10]  José Humberto S. Almeida,et al.  Waviness and fiber volume content analysis in continuous carbon fiber reinforced plastics made by tailored fiber placement , 2019, Composite Structures.

[11]  K. Gliesche,et al.  3D reinforced stitched carbon/epoxy laminates made by tailored fibre placement , 2000 .

[12]  A. Malakhov,et al.  Design of composite structures reinforced curvilinear fibres using FEM , 2016 .

[13]  José Humberto S. Almeida,et al.  Optimizing Variable-Axial Fiber-Reinforced Composite Laminates: The Direct Fiber Path Optimization Concept , 2019, Mathematical Problems in Engineering.

[14]  T. Nomura,et al.  Cross-section optimization of topologically-optimized variable-axial anisotropic composite structures , 2019, Composite Structures.

[15]  Michael R Wisnom,et al.  An experimental and numerical investigation into the damage mechanisms in notched composites , 2009 .

[16]  G. Heinrich,et al.  Using tailored fibre placement technology for stress adapted design of composite structures , 2008 .

[17]  M. Wisnom,et al.  An experimental investigation into size effects in quasi-isotropic carbon/epoxy laminates with sharp and blunt notches , 2014 .

[18]  M. Wisnom,et al.  Size effects in unnotched tensile strength of unidirectional and quasi-isotropic carbon/epoxy composites , 2008 .

[19]  F. Pires,et al.  Fibre steering for shear-loaded composite panels with cutouts , 2014 .

[20]  Paul M. Weaver,et al.  Continuous tow shearing for manufacturing variable angle tow composites , 2012 .

[21]  Zafer Gürdal,et al.  Tailoring for strength of composite steered-fibre panels with cutouts , 2010 .

[22]  Joël Cugnoni,et al.  Thin ply composites: Experimental characterization and modeling of size-effects , 2014 .

[23]  M. W. Hyer,et al.  Use of curvilinear fiber format in composite structure design , 1991 .

[24]  Pedro P. Camanho,et al.  Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear , 2006 .

[25]  I. Herszberg,et al.  Tailored fibre placement to minimise stress concentrations , 1997 .

[26]  Volnei Tita,et al.  Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout , 2019, Composite Structures.

[27]  Z. Hashin Failure Criteria for Unidirectional Fiber Composites , 1980 .

[28]  Paul M. Weaver,et al.  Manufacturing characteristics of the continuous tow shearing method for manufacturing of variable angle tow composites , 2014 .

[29]  J. Llorca,et al.  X-ray computed tomography analysis of damage evolution in open hole carbon fiber-reinforced laminates subjected to in-plane shear , 2016 .

[30]  Tong Earn Tay,et al.  Numerical analysis of size effects on open-hole tensile composite laminates , 2013 .

[31]  F. Chang,et al.  Modelling of splitting and delamination in notched cross-ply laminates , 2000 .

[32]  N. Gascons,et al.  Variable-stiffness composite panels: Defect tolerance under in-plane tensile loading , 2014 .

[33]  Mehdi Shahbazi,et al.  Determination of material properties for ANSYS progressive damage analysis of laminated composites , 2017 .