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Interlaminar Fracture Toughness of Quasibrittle Composites Under Crack-Parallel Tension

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Title: Interlaminar Fracture Toughness of Quasibrittle Composites Under Crack-Parallel Tension

Authors: Genki Matsubara, Gaurav Joshi, Marco Salviato

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Abstract: Recent research challenges the traditional LEFM assumption that crack-parallel stresses have minimal impact on fracture toughness. Gap Test results reveal that in quasibrittle materials, Mode I fracture energy is significantly affected by crack-parallel compression. While compressive stress increases fracture energy up to a point, it eventually leads to a reduction near the material’s compressive strength. In carbon fiber laminates, intra-laminar fracture energy decreases steadily under parallel compression. The Crack Band Model (CBM) effectively captures this behavior, unlike Cohesive Zone Models (CZMs), which fell short to represent the finite-thickness Fracture Process Zone (FPZ). Building on this, we introduce the Half Open I test, a novel method to assess Mode I interlaminar fracture energy under crack-parallel tensile stress. The test uses localized moments at the crack opening to evaluate fracture energy, revealing how tensile stress affects FPZ size and total fracture energy. This new approach corrects previous over/under-estimations in fracture toughness and offers more accurate predictions for the integrity of quasibrittle composite structures.

References: 1. S Rana and R Fangueiro. “Advanced composites in aerospace engineering”. In: Advanced composite materials for aerospace engineering. Elsevier, 2016, pp. 1–15. 2. IN WIND. “Structural Analysis of Composite Wind Turbine Blades”. 3. Ahmed Elmarakbi. Advanced composite materials for automotive applications: Structural integrity and crashworthiness. John Wiley & Sons, 2013. 4. Chiara Ceccato et al. “Simulation of concrete failure and fiber reinforced polymer fracture in confined columns with different cross sectional shape”. In: International Journal of Solids and Structures 108 (2017), pp. 216–229. 5. Jeremy Brockmann and Marco Salviato. “The gap test–effects of crack parallel compression on fracture in carbon fiber composites”. In: Composites Part A: Applied Science and Manufacturing 164 (2023), p. 107252. 6. Victor Giurgiutiu. Stress, vibration, and wave analysis in aerospace composites: SHM and NDE applications. Academic Press, 2022. ISBN: 978-0-12-813308-8. 7. Airbus SAS. Boeing 787: Lessons Learnt. Accessed: January 16, 2025. 2008. URL: http://wpage.unina.it/fabrnico/DIDATTICA/PGV_2012/MAT_DID_CORSO/Design_Cases/ Boeing_787_Lessons_learnt.pdf 8. Masaki Hojo et al. “Modes I and II interlaminar fracture toughness and fatigue delamination of CF/epoxy laminates with self-same epoxy interleaf”. In: International Journal of Fatigue 28.10 (2006), pp. 1154–1165. 9. D Paul et al. “Evolution of US military aircraft structures technology”. In: Journal of Aircraft 39.1 (2002), pp. 18–29. 10. C Frey, S Dölling, and W Becker. “Closed-form analysis of interlaminar crack initiation in angle-ply laminates”. In: Composite Structures 257 (2021), p. 113060. 11. Zdeněk P Bažant, Jia-Liang Le, Marco Salviato, et al. Quasibrittle fracture mechanics and size effect: A first course. Oxford University Press, 2021. 12. Marco Salviato et al. “A novel discrete, mesoscale modeling framework for the simulation of the damaging and fracturing behavior of composites”. In: ASME International Mechanical Engineering Congress and Exposition. Vol. 86717. American Society of Mechanical Engineers. 2022, V009T12A015. 13. Marco Salviato et al. “To the mesoscale and beyond! capturing complex damage mechanisms in composites via simple, physics-based, discrete mathematical models of fibers and matrix”. In: Proceedings of the American Society for Composites–Thirty-Eighth Technical Conference, 2023. 14. Zdeněk P. Bažant and J. Planas. Fracture and Size Effect in Concrete and Other Quasibrittle Materials. CRC Press, 1998. 15. Hoang Nguyen et al. “New perspective of fracture mechanics inspired by gap test with crackparallel compression”. In: Proceedings of the National Academy of Sciences 117.25 (2020), pp. 14015–14020. 16. Yuhui Lyu et al. “Dissipation mechanisms of crack-parallel stress effects on fracture process zone in concrete”. In: Journal of the Mechanics and Physics of Solids 181 (2023), p. 105439. 17. EK Tschegg, M Elser, and SE Stanzl-Tschegg. “Biaxial fracture tests on concrete— Development and experience”. In: Cement and Concrete Composites 17.1 (1995), pp. 57–75. 18. Linfei Li et al. “Crack-Parallel Stress Effect on Fracture of Fiber-Reinforced Concrete Revealed by Gap Tests”. In: Journal of Engineering Mechanics 150.4 (2024), p. 04024011. 19. Christos Kassapoglou. Design and analysis of composite structures: with applications to aerospace structures. John Wiley & Sons, 2013. 20. Alan A Baker. Composite materials for aircraft structures. AIAA, 2004. 21. John T Wang. “Continuum Damage Mechanics Based Explicit 3D Progressive Failure Analysis of Composite Laminates”. In: The Aircraft Airworthiness and Sustainment Conference. NF1676L-21070. 2015. 22. Stephen B Clay and Philip M Knoth. “Experimental results of quasi-static testing for calibration and validation of composite progressive damage analysis methods”. In: Journal of Composite Materials 51.10 (2017), pp. 1333–1353. 23. Michael C. Y. Niu. Airframe Structural Design. Hong Kong: Conmilit Press Ltd., 1988. ISBN: 9627128082. 24. N Shama Rao et al. “Carbon composites are becoming competitive and cost effective”. In: White Paper (2018). 25. João Pedro Cunha Pinto. “Economic comparison between materials in the aerospace industry”. In: Tecnico Lisboa (2017). 26. Yagmur Atescan-Yuksek et al. “Comparative life cycle assessment of aluminium and CFRP composites: the case of aerospace manufacturing”. In: The International Journal of Advanced Manufacturing Technology 131.7 (2024), pp. 4345–4357. 27. I Bianchi et al. “Development and Life Cycle Analyses of Carbon Fiber Reinforced Polymer Tubular Parts for Metal Replacement in Aerospace Applications”. In: Journal of Materials Engineering and Performance (2025), pp. 1–12. 28. Stephen W Tsai and José Daniel D Melo. Composite materials design and testing: Unlocking mystery with invariants. Composites Design Group Stanford, UK, 2015. 29. Zdeněk P Bažant, R Gettu, and MT Kazemi. “Identification of nonlinear fracture properties from size effect tests and structural analysis based on geometry-dependent R-curves”. In: International Journal of Rock Mechanics and Mining Sciences & Geomechanics Abstracts 28.1 (1991), pp. 43–51. 30. Yeoushang Jenq and Surendra P Shah. “Two parameter fracture model for concrete”. In: Journal of Engineering Mechanics 111.10 (1985), pp. 1227–1241. 31. P Weißgraeber, S Hell, and W Becker. “Crack nucleation in negative geometries”. In: Engineering Fracture Mechanics 168 (2016), pp. 93–104. 32. Syensqo. CYCOM® 977-3 – 350°F (177°C) curing toughened epoxy resin. https://www.syensqo.com/en/product/cycom-977-3. Accessed: 2025-07-10. 33. Zünd Systemtechnik AG. G3 Digital Cutting System. Accessed: July 11, 2025. URL: https://www.zund.com/en/cutting-systems/digitalcutting-systems/g3-cutter. 34. University of Washington. Advanced Composites Center. 2025. URL: https://www.uwacc.uw.edu/ (visited on 02/02/2025). 35. Rachael Geerts. Vacuum Bagging Basics. Epoxyworks. Published online, accessed 2025-0710, https://www.epoxyworks.com/vacuum-bagging-basics/. 36. Jiacheng Chen. “Comprehensive Investigation of Quasibrittle Fracture of IM7/977- 3 Laminates via Size Effect Analysis”. MA thesis. University of Washington, 2023, p. 88. 37. ASTM International. Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites. Developed by Subcommittee D30.06. ICS Code: 83.120. West Conshohocken, PA: ASTM International, 2013. DOI: 10.1520/D5528-13.

Conference: SAMPE 2026

Publication Date: 2026/04/27

SKU: 159

Pages: 11

Price: $22.00

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