Slow-growth damage tolerance for fatigue after impact in FRP composites: Why current research won’t get us there

Abstract Impact damage in CFRP structures is currently managed using the ‘no-growth’ concept, meaning that damage is not allowed to grow under fatigue loading. This requires that stresses in the material are kept below the fatigue limit, imposing a significant weight penalty. A ‘slow-growth’ concept would allow more efficient structural designs, but several knowledge gaps need to be addressed before this is possible. These gaps exist in three main areas: (1) damage characterisation, (2) fatigue driven delamination growth after impact, and (3) final failure of impacted laminates. The paper highlights open questions and the shortcomings of current research in addressing them, and suggests avenues for future research.

[1]  M. A. Verges,et al.  X-ray computed microtomography of internal damage in fiber reinforced polymer matrix composites , 2005 .

[2]  L. Molent,et al.  A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment , 2020 .

[3]  Libin Zhao,et al.  An extended analytical model for predicting the compressive failure behaviors of composite laminate with an arbitrary elliptical delamination , 2020 .

[4]  O. Falcó,et al.  An efficient numerical approach to the prediction of laminate tolerance to Barely Visible Impact Damage , 2019, Composite Structures.

[5]  S. Hallett,et al.  Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI): Experimental and numerical study , 2018 .

[6]  F. Meer,et al.  Cohesive zone and level set method for simulation of high cycle fatigue delamination in composite materials , 2017 .

[7]  M. Mitrovic Effect of loading parameters on the fatigue behavior of impact damaged composite laminates , 1999 .

[8]  L. Melin,et al.  Fatigue testing and buckling characteristics of impacted composite specimens , 2002 .

[9]  K. Kunoo,et al.  Compression fatigue failure of CFRP laminates with impact damage , 2009 .

[10]  Xiaodong He,et al.  Delamination growth behavior in carbon fiber reinforced plastic angle ply laminates under compressive fatigue loads , 2012 .

[11]  S. C. Galea,et al.  The development of fatigue damage around fastener holes in thick graphite/epoxy composite laminates , 1993 .

[12]  L. Banks‐Sills,et al.  Multi-directional composite laminates: fatigue delamination propagation in mode I—a comparison , 2019, International Journal of Fracture.

[13]  M. Shokrieh,et al.  Development of a physics-based theory for mixed mode I/II delamination onset in orthotropic laminates , 2019, Theoretical and Applied Fracture Mechanics.

[14]  A. Nettles,et al.  The Influence of GI and GII on the compression after impact strength of carbon fiber/epoxy laminates , 2017 .

[15]  R. Alderliesten,et al.  Cyclic fatigue fracture of composites: What has testing revealed about the physics of the processes so far? , 2018, Engineering Fracture Mechanics.

[16]  Chris Williams,et al.  The detection, inspection, and failure analysis of a composite wing skin defect on a tactical aircraft , 2013 .

[17]  S. Pinho,et al.  Interlocking thin-ply reinforcement concept for improved fracture toughness and damage tolerance , 2019, Composites Science and Technology.

[18]  A. Mouritz,et al.  Compression fatigue properties of z-pinned quasi-isotropic carbon/epoxy laminate with barely visible impact damage , 2011 .

[19]  Esben Lindgaard,et al.  A simulation method for fatigue-driven delamination in layered structures involving non-negligible fracture process zones and arbitrarily shaped crack fronts , 2019, Composites Part A: Applied Science and Manufacturing.

[20]  Darryl P Almond,et al.  Impact damage growth in composites under fatigue conditions monitored by acoustography , 2002 .

[21]  J. Botsis,et al.  Influence of ply-angle on fracture in antisymmetric interfaces of CFRP laminates , 2019, Composite Structures.

[22]  R. Benedictus,et al.  Characterizing fatigue delamination growth behaviour using specimens with multiple delaminations: The effect of unequal delamination lengths , 2013 .

[23]  Rinze Benedictus,et al.  Methods for the prediction of fatigue delamination growth in composites and adhesive bonds: A critical review , 2013 .

[24]  Rinze Benedictus,et al.  Towards a physics-based relationship for crack growth under different loading modes , 2018 .

[25]  A. P. Vassilopoulos,et al.  Experimental investigation of two-dimensional delamination in GFRP laminates , 2018, Engineering Fracture Mechanics.

[26]  P. Irving,et al.  Impact, post-impact strength and post-impact fatigue behaviour of polymer composites , 2015 .

[27]  Takashi Ishikawa,et al.  Fatigue behavior and lifetime distribution of impact-damaged carbon fiber/toughened epoxy composites under compressive loading , 2013 .