On crack tunneling and plane-strain delamination in laminates
Source abstract
Abstract
Previous numerical work on crack tunnelling and plane-strain delamination in layered solids is evaluated with static and fatigue experiments and analysis. It is concluded that the translation of the theory derived for static fracture to fatigue loading is not as straightforward as initially assumed. Details such as delamination location, stress state, plasticity and mode-mixity need further consideration to obtain a theory that is sufficiently adequate to describe the static and fatigue phenomena observed in practice.
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Research context
OpenAlex topics: Ultrasonics and Acoustic Wave Propagation · Mechanical Behavior of Composites · Numerical methods in engineering
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (39)
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1. Alderliesten RC (2005) Fatigue crack propagation and delamination growth in Glare. PhD dissertation, Delft University of Technology, 2005
2. Alderliesten RC (2007a) Analytical prediction model for fatigue crack propagation and delamination growth in Glare. Int J Fatigue 29: 628–64610.1016/j.ijfatigue.2006.07.006 ↗
3. Alderliesten RC (2007b) Damage tolerance of bonded aircraft structures. In: Proceedings of the 1st international conference on damage tolerance of aircraft structures, Delft, The Netherlands, 2007
4. Alderliesten RC, Schijve J, van der Zwaag S (2006) Application of the energy release rate approach for delamination growth in Glare. Eng Fract Mech 73(6): 697–70910.1016/j.engfracmech.2005.10.006 ↗
5. Alderliesten RC, Campoli G, Benedictus R (2007) Modelling cyclic shear deformation of fibre/epoxy layers in fibre metal laminates. Compos Sci Technol 67(11–12): 2545–255510.1016/j.compscitech.2006.12.011 ↗
6. ASTM International (2001) D 6671/D 6671M-06, Standard Test Method for Mixed Mode I–Mode II Interlaminar Fracture Toughness of Unidirectional Fiber Reinforced Polymer Matrix Composites. Annual Book of ASTM Standards, volume 15.03, 2001
7. Beumler Th (2004) Flying Glare®, a contribution to aircraft certification issues on strengths properties in non-damaged and fatigue damaged GLARE® structures. PhD dissertation, Delft University of Technology, Delft
8. Chan KS, He M-Y, Hutchinson JW (1993) Cracking and stress redistribution in ceramic layered composites. Mater Sci Eng A 167: 57–6410.1016/0921-5093(93)90337-E ↗
9. de Vries TJ (2001) Blunt and sharp notch behaviour of Glare laminates. PhD dissertation, Delft University of Technology, 2001
10. de Vries TJ, Vlot A, Hashagen F (1999) Delamination behavior of spliced fiber metal laminates, Part 1—experimental results. Compos Struct 46(2): 131–14510.1016/S0263-8223(99)00049-5 ↗
11. Dollar A, Steif PS (1991) The branched crack problem revisited. J Appl Mech (ASME) 58: 584–58610.1115/1.2897227 ↗
12. Ewalds HL, Wanhill RJH (1984) Fracture mechanics. Delftse Uitgevers Maatschappij, Delft
13. Forman RG, Kearney VE, Engle RM (1967) Numerical analysis of crack propagation in cyclic loaded structures. J Basic Eng Trans ASME 89: 459–46410.1115/1.3609637 ↗
14. Fracture Mechanics and Fatigue Crack Growth Analysis Software NASGRO®, version 5.2 (2008) Southwest Research Institute, P.O. Drawer 28510, San Antonio, Texas 78228-0510
15. Guo YJ, Wu XR (1998) A theoretical model for predicting fatigue crack growth rates in fibre-reinforced metal laminates. Fatigue Fract Eng Mater Struct 21: 1133–114510.1046/j.1460-2695.1998.00076.x ↗
16. Guo YJ, Wu XR (1999) Bridging stress distribution in center-cracked fiber reinforced metal laminates: modelling and experiment. Eng Fract Mech 63: 147–16310.1016/S0013-7944(99)00018-1 ↗
17. Hart-Smith LJ (1973) Adhesive-bonded single lap joints, Langley Research Center, NASA CR-112236, Hampton, Virginia
18. He M-Y, Hutchinson JW (1989) Crack deflection at an interface between dissimilar elastic materials. Int J Solids Struct 25(9): 1053–106710.1016/0020-7683(89)90021-8 ↗
19. Hooijmeijer PA (2002) Doubler run-out fatigue properties. Report B2V-02-16, Delft University of Technology, 2002 (restricted)
20. Lee J, Kim H (2005) Stress analysis of generally asymmetric single lap adhesively bonded joints. J Adhes 81: 443–47210.1080/00218460590944918 ↗
21. Lu TJ (1996) Crack branching in all-oxide ceramics composites. J Am Ceramics 79: 266–27410.1111/j.1151-2916.1996.tb07908.x ↗
22. Marissen R (1988) Fatigue crack growth in ARALL, a hybrid Aluminium-Aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. PhD thesis, Delft University of Technology
23. Paris PC, Erdogan F (1963) A critical analysis of crack propagation laws. Trans ASME Ser D 85: 528–53510.1115/1.3656900 ↗
24. Plokker HM, Alderliesten RC, Benedictus R (2007) Crack closure in fibre metal laminates. Fatigue Fract Eng Mater Struct 30: 608–62010.1111/j.1460-2695.2007.01140.x ↗
25. Priddle EK (1972) High cycle fatigue crack propagation under random and constant amplitude loadings. Int J Press Vessels Piping 4: 8910.1016/0308-0161(76)90014-4 ↗
26. Qin M, Dzenis YA (2003) Analysis of single lap adhesive composite joint with delaminated adherends. Compos Part B 34(2): 167–17310.1016/S1359-8368(02)00066-5 ↗
27. Roebroeks GHJJ (1991) Towards GLARE—the development of and fatigue insensitive and damage tolerant aircraft material. PhD thesis, Delft University of Technology
28. Roebroeks GHJJ, Hooijmeijer PA, Kroon EJ, Heinimann MB (2007) The development of Central. In: Proceedings of the 1st international conference on damage tolerance of aircraft structures, Delft, The Netherlands, 2007
29. Schijve J (1972) Some elementary calculations on secondary bending in simple lap joints, NLR-TR-72036, National Aerospace laboratory, Amsterdam, The Netherlands
30. Schijve J (2001) Fatigue of structures and materials. Kluwer Academic Publishers, Dordrecht
31. Schijve J, Van Lipzig HTM, Van Gestel GFJA, Hoeymakers AHW (1979) Fatigue properties of adhesive-bonded laminated sheet material of aluminium alloys. Eng Fract Mech 12: 561–57910.1016/0013-7944(79)90098-5 ↗
32. Setoodeh AR, Hadavinia H, Biglari FR, Nikbin K (2005) Comparison of analytical, numerical, and experimental methods in deriving fracture toughness properties of adhesives using bonded double lap joint specimens. J Adhes 81: 529–55310.1080/00218460590944963 ↗
33. Suiker ASJ, Fleck NA (2004) Crack tunnelling and plane-strain delamination in layered solids. Int J Fract 125: 1–3210.1023/B:FRAC.0000021064.52949.e2 ↗
34. Suiker ASJ, Fleck NA (2006) Modelling of fatigue crack tunneling and delamination in layered composites. Compos Part A 37: 1722–173310.1016/j.compositesa.2005.09.006 ↗
35. Tada H, Paris PC, Irwin GR (2000) The stress analysis of cracks handbook, 3rd edn. The American Society of Mechanical Engineers10.1115/1.801535 ↗
36. Takamatsu T, Matsumura T, Ogura N, Shimokawa T, Kakuta Y (1999) Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate. Eng Fract Mech 63: 253–27210.1016/S0013-7944(99)00021-1 ↗
37. Takamatsu T, Shimokawa T, Matsumura T, Miyoshi Y, Tanabe Y (2003) Evaluation of fatigue crack growth behaviour of GLARE3 fiber/metal laminates using compliance method. Eng Fract Mech 70: 2603–261610.1016/S0013-7944(03)00063-8 ↗
38. Thomas H, Mitrovic M, Turkgenc O (1999) The effect of loading parameters on fatigue of composite laminates: part III. Report DOT/FAA/AR-99/22, U.S. Department of Transportation, Federal Aviation Administration, Office of Aviation Research, Washington, DC 20591
39. Tong L (1996) Bond strength for adhesive-bonded single-lap joints. Acta Mech 117: 101–11310.1007/BF01181040 ↗