A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment

Rouchon J. (1995) Fatigue and damage tolerance aspects for composite aircraft structures, ICAF symposium – Delft TN, March 1995 ICAF-DOC-2051. Breaking news: Mitsubishi drops composite wing from own jet project, https://blogs.crikey.com.au/planetalking/2009/09/10/787-breaking-news-mitsubishidrops-composite-wing-from-own-jet-project. Stinchcomb WW, Bakis CE, Chapter 4 – Fatigue Behavior of Composite Laminates. In: Reifsnider KL, editor. Composite Materials Series, vol. 4, Elsevier; 1991, p. 105–80. doi:10.1016/B978-0-444-70507-5.50008-1. Reifsneider KL, Chapter 2 – Damage and Damage Mechanics. In: Reifsnider KL, editor. Composite Materials Series, vol. 4, Elsevier; 1991, p. 11–77. doi:10.1016/B978-0-444-70507-5.50006-8. Iarve, 2017, Progressive failure simulation in laminated composites under fatigue loading by using discrete damage modelling, Composite Mater, 51, 2143, 10.1177/0021998316681831 Clay, 2016, Benchmarking of composite progressive damage analysis methods: the background, J Compos Mater., 51, 1325, 10.1177/0021998316672520 Justusson B, Schaefer J, Liguore S, Holzwarth R. Assessment of state of the art composite progressive damage and failure analysis methods for aircraft structural durability applications, proc. Aircraft Structural Integrity Program Conference, November 26-29, 2018, Phoenix AZ. Nikishkov Y, Nikishkov G, Seon G, Shonkwiler B, Makeev A. Structures Technology for Component Damage and Failure Prediction, proc. Vertical Flight Society’s 75th Annual Forum and Technology Display, Philadelphia, PA, USA, May 13-16, 2019. Krueger R, Carvalho N. In search of a time efficient approach to crack and delamination growth prediction in composites, NIS, NASA, VA USA, 2016. Dávila CG, From S-N to the Paris law with a new mixed-mode cohesive fatigue model, NASA/TP–2018-219838, Jun 2018. Jones, 1985, Compression failures of damaged graphite epoxy laminates, Compos Struct, 3, 167, 10.1016/0263-8223(85)90042-X Molent, 2017, The lead crack concept applied to defect growth in aircraft composite structures, Compos Struct, 166, 22, 10.1016/j.compstruct.2016.12.076 Cvitkovich, 1997 Bisagni C, Furfari D, Pacchione M. Fatigue and Damage Tolerance Assessment of 3-D reinforced CFRP Bonded Joints, 28th ICAF Symposium, Helsinki, 3–5 June 2015. Chen, 2006, A comparison of total fatigue life models for composite laminates, Fatigue Fract Engng Mater Struct, 29, 31, 10.1111/j.1460-2695.2006.00958.x Goh, 2014, Effect of disbonds on the fatigue endurance of composite scarf joints, Adv Mater Res, 891–892, 191, 10.4028/www.scientific.net/AMR.891-892.191 Lin, 1996, Fatigue delamination growth in carbon fibre-reinforced aluminium laminates, Composites, A 2lA, 9, 10.1016/1359-835X(95)00006-N Mohlin T, Blom AF, Carlsson LA, Gustasvsson AI. (1985) Delamination growth in a notched graphie/epoxy laminate under compression fatigue loading, Delamination and Debonding of Materials, ASTM STP 876, Ed. W.S. Johnson, Philadelphia, pp 168–188. Han, 2001 Han HT, Mitrovic M, Turkgenc O. The Effect of Loading Parameters on Fatigue of Composite Laminates: Part III, DOT/FAA/AR-99/22, Jun 1999, Washington. USA. Chang JB, Goyal VK, Klug JC, Rome JI. (2012), Composite Structures Damage Tolerance Analysis Methodologies, NASA/CR-2012-217347, Virginia, USA. Kantzos, 1989 Jones, 1989, Thermoelastic assessment of damage growth in composites, Compos Struct, 12, 291, 10.1016/0263-8223(89)90077-9 Pettit DE, Lauraitus KN, Cox JM. Advanced residual strength degradation rate modelling for advanced composite structures, Volume 1 – Task I: Preliminary Screening, AFWAL-TR-79-3095, Wright-Patterson Air Force Base, Ohio, Aug 1979. Jones, 2017, Delamination growth in polymer-matrix fibre composites and the use of fracture mechanics data for material characterisation and life prediction, Compos Struct, 180, 316, 10.1016/j.compstruct.2017.07.097 Rouchon, 2009 Brandecker B, Higert R. (1988) A320 full scale structural testing for fatigue and damage tolerance certification of metallic and composite structure, ICAS-88-5.8.1. Saunders, 1990, Graphite/epoxy laminate coupon testing programme, Theor Appl Fract Mech, 13, 105, 10.1016/0167-8442(90)90029-Y