A mixed-mode fatigue crack growth model for co-consolidated thermoplastic joints

1. 2020

2. Adhesive Bonding of Aircraft Structures

3. A Literature Review on Crack Arrest Features for Composite Materials and Composite Joints with a Focus on Aerospace Applications10.3390/aerospace10020137 ↗

4. European Aviation Safety Agency E. AMC 20-29 Composite Aircraft Structure 2010;Annex II to ED Decision 2010/003/R of 19/07/2010.

5. Fatigue behavior of hybrid and bonded single lap joints made of composite material10.1016/j.prostr.2022.05.071 ↗

6. Experimental characterization of Mode I fatigue delamination growth onset in composite joints: A comparative study10.1016/j.matdes.2018.10.007 ↗

7. A progressive damage model for composite laminates based on non-linear continuum mechanics—Static and fatigue loadings10.1016/j.tafmec.2022.103639 ↗

8. A study on fatigue crack propagation in thick composite adhesively bonded joints10.1016/j.ijfatigue.2012.05.018 ↗

9. Experimental evaluation of Refill friction Stir spot Welds (RFSSW) as crack arrest features in co-consolidated thermoplastic laminates10.1016/j.compstruct.2023.116754 ↗

10. Fatigue response of ultrasonically welded carbon/Elium® thermoplastic composites10.1016/j.matlet.2020.127362 ↗

11. Dynamic analysis of scarf adhesive joints in CFRP composites modified with Al2O3-nanoparticles under fatigue loading at different temperatures10.1016/j.compositesa.2021.106277 ↗

12. Sioutis I, Tsiangou E, Allègre F, Boutin H, Plassot H, Tserpes K, et al. Characterization and simulation of the mechanical response of co-consolidated thermoplastic cracked lap shear joints containing two novel disbond arrest features. In: Proceedings of the 20th European Conference on Composite Materials, vol. 4, Lausanne, Switzerland: n.d., p. 982–9. http://dx.doi.org/10.5075/epfl-298799_978-2-9701614-0-0.

13. Fatigue crack simulation of the 316L brazed joint using the virtual crack closure technique10.1016/j.ijpvp.2019.04.018 ↗

14. An XFEM-VCCT coupled approach for modeling mode I fatigue delamination in composite laminates under high cycle loading10.1016/j.engfracmech.2021.107760 ↗

15. A new approach to model delamination growth in fatigue using the Virtual Crack Closure Technique without re-meshing10.1016/j.engfracmech.2019.106614 ↗

16. An efficient and versatile use of the VCCT for composites delamination growth under fatigue loadings in 3D numerical analysis: the Sequential Static Fatigue algorithm10.1016/j.ijfatigue.2022.107493 ↗

17. A cohesive model of fatigue crack growth10.1023/A:1010839522926 ↗

18. A cohesive zone model to predict fatigue-driven delamination in composites10.1016/j.engfracmech.2020.107124 ↗

19. Cohesive zone model for high-cycle fatigue of composite bonded joints under mixed-mode I+II loading10.1016/j.engfracmech.2015.03.044 ↗

20. Numerical evaluation of crack stopping mechanisms in composite bonded joints due to corrugation and bolts10.1051/matecconf/201930401003 ↗

21. Numerical simulation of quasi-static and fatigue debonding growth in adhesively bonded composite joints containing bolts as crack stoppers10.1080/00218464.2019.1690473 ↗

22. A review on failure theories and simulation models for adhesive joints10.1080/00218464.2021.1941903 ↗

23. Numerical simulation of fatigue-driven delamination using interface elements10.1002/nme.1338 ↗

24. Cohesive zone length in numerical simulations of composite delamination10.1016/j.engfracmech.2008.06.004 ↗

25. A fatigue degradation law for cohesive interface elements – Development and application to composite materials10.1016/j.ijfatigue.2010.04.006 ↗

26. Simulation of delamination in composites under high-cycle fatigue10.1016/j.compositesa.2006.11.009 ↗

27. A crack tip tracking algorithm for cohesive interface element analysis of fatigue delamination propagation in composite materials10.1016/j.ijsolstr.2012.03.034 ↗

28. Fatigue crack growth simulation in adhesively bonded composite joints10.1111/ffe.12969 ↗

29. Fatigue damage modelling of adhesively bonded joints under variable amplitude loading using a cohesive zone model10.1016/j.engfracmech.2011.09.008 ↗

30. Russel · 1989 · 162

31. ASTM International. D 5528 – 01 Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites n.d.

32. Fatigue crack growth characterization in adhesive CFRP joints10.1016/j.compstruct.2018.09.020 ↗

33. Airbus Industrie Test Method. AITM 1.0006 Determination of interlaminar fracture toughness energy Mode II. Blagnac Cedex France: 1994.

34. D14 Committee. Test Method for Lap Shear Adhesion for Fiber Reinforced Plastic (FRP) Bonding. ASTM International; n.d. https://doi.org/10.1520/D5868-01R14.10.1520/D5868-01R14 ↗

35. Numerical simulation of debonding of a composite-to-metal adhesive joint subjected to centrifugal load10.1016/j.engfailanal.2022.106131 ↗

36. Development and Numerical Implementation of a Modified Mixed-Mode Traction–Separation Law for the Simulation of Interlaminar Fracture of Co-Consolidated Thermoplastic Laminates Considering the Effect of Fiber Bridging10.3390/ma15155108 ↗

37. Sioutis I, Tserpes K. A modified cohesive zone model for the simulation of mixed-mode fracture of co-consolidated thermoplastic laminates considering fiber bridging. 8th European Congress on Computational Methods in Applied Sciences and Engineering, CIMNE; 2022. https://doi.org/10.23967/eccomas.2022.018.10.23967/eccomas.2022.018 ↗