journal article·2013-01Open access

Mixed-mode fatigue crack growth in FM73 bonded joints

T.A. Hafiz, M.M. Abdel-Wahab, A.D. Crocombe, P.A. Smith

Abstract

Abstract Fatigue tests have been carried out to investigate mixed mode fatigue crack growth behaviour in FM73 epoxy adhesive using double cantilever beam (DCB) specimens. The DCB configuration used consisted of equal thickness mild steel adherends bonded with FM73 adhesive. The joints were tested under pure mode I and a range of fatigue mixed-mode conditions using a relatively simple, variable-mode loading fixture developed in previous work [1]. The fatigue testing was carried out in displacement control, with an initial load ratio ( R ) of 0.1. The fatigue load decreased as the fatigue crack grew and this load was recorded. Crack growth was monitored and measured using a video microscope. The results suggest that crack initiation in the test specimens is controlled by the mode I strain energy release rate, G I component. The fatigue crack growth rates were characterised using a Paris law approach, from which it appears that the total strain energy release rate range, Δ G Total , is a more dominant factor in controlling crack growth than the mode I component of strain energy release rate range, ΔG I . For a quantitative description of the mixed-mode fatigue crack growth, generalised forms of the Paris relation are developed.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Ultrasonics and Acoustic Wave Propagation

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (30)

Show source-provided references
1. Mixed-mode fracture of adhesively bonded metallic joints under quasi-static loading10.1016/j.engfracmech.2010.09.015 ↗
2. Mixed mode I/II Fatigue crack growth in adhesive joints10.1016/j.engfracmech.2006.04.009 ↗
3. Kinloch · 1987
4. Mostovoy · 1975
5. Hertzberg · 1995
6. Elber · 1971
7. A fracture mechanics study of the influence of moisture on the fatigue behaviour of adhesively bonded aluminium joints10.1016/0143-7496(96)89799-5 ↗
8. The fatigue and durability of automotive adhesives. Part I: fracture mechanics tests10.1080/00218469708010517 ↗
9. The role of the interphase in the environmental failure of adhesive joints10.1016/S1359-6454(00)00240-8 ↗
10. Frequency effect on fatigue crack growth rate in joints with either filled or filled and toughened adhesive10.1016/0142-1123(95)93540-I ↗
11. Observations of fatigue crack initiation and propagation in an epoxy adhesive10.1016/S0143-7496(96)00044-9 ↗
12. Interface crack growth in layered materials
13. On the calculation of energy release rate for cracked laminates10.1007/BF00017790 ↗
14. T.A. Hafiz, Mixed-mode fracture in adhesively bonded joints under quasi-static and fatigue loading. PhD thesis, University of Surrey, UK.
15. Fatigue crack growth in bonded DCB specimens10.1016/S0013-7944(03)00046-8 ↗
16. Usermanual, Instron 8511. High Wycombe: Instron
17. Mode I fracture of epoxy bonded composite joints: part1. Quasi-static loading10.1016/S0143-7496(00)00038-5 ↗
18. Hertzberg · 1980
19. Ripling EJ, Crosley PB, Johnson WS. A comparison of pure mode I and mixed mode I-III cracking of an adhesive containing an ope nknit cloth carrier Adhesively bonded joints: testing,analysis and design, ASTM STP 981. Ed. Johnson WS, editor. ASTM; 1988. p.163-82.10.1520/STP30335S ↗
20. Johnson WS, Lawrence MB, Rodolfo VV. Application of fracture mechanics to the durability of bonded composite joints. Report No. DOT/FAA/AR-97/56; 1998.
21. Fracture mechanics and damage mechanics based fatigue lifetime prediction of adhesively bonded joints subjected to variable amplitude fatigue10.1016/j.engfracmech.2010.03.008 ↗
22. Ramkumar · 1985
23. Delamination fatigue crack growth in unidirectional graphite/epoxy laminates10.1177/073168448700600104 ↗
24. Russell · 1989
25. Delamination growth in composites under cyclic loads10.1177/002199839402800803 ↗
26. Growth of internal delaminations under cyclic compression in composite plates10.1016/0022-5096(95)00012-8 ↗
27. Mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites under fatigue loading10.1016/S0266-3538(97)00021-3 ↗
28. Model of delamination propagation in brittle-matrix composites under cyclic loading10.1177/073168401772678742 ↗
29. Mixed-mode delamination growth in carbon–fibre composite laminates under cyclic loading10.1016/j.ijsolstr.2004.02.040 ↗
30. Johnson WS, Mangalgiri PD. Influence of the resin on interlaminar mixed-mode fracture, toughened composites In: ASTM STP 937; Ed. Johnston NJ, Philadelphia, 1987. p. 295–31510.1520/STP24384S ↗