Effects of fibre/matrix adhesion on carbon-fibre-reinforced metal laminates - I. residual strength

Composites Science and Technology

Volumn 57, Issue 12, 1998, Pages 1609-1619

  Lawcock, G D ^a   Ye, L ^a   Mai, Y W ^a   Sun, C T ^b  

^a UNIVERSITY OF SYDNEY   (Australia)

^b Purdue University   (United States)

Author keywords

A. layered structures; B. fibre matrix bond; Damage mechanisms; Fibre surface treatment; Residual strength

Indexed keywords

ADHESION; CARBON FIBERS; DELAMINATION; ELASTIC MODULI; FAILURE (MECHANICAL); FRACTURE MECHANICS; INTERFACES (MATERIALS); LAMINATED COMPOSITES; MECHANICAL TESTING; RESIDUAL STRESSES; SCANNING ELECTRON MICROSCOPY; SHEAR STRENGTH;

CARBON FIBER REINFORCED METAL LAMINATES; DAMAGE MECHANISM; FIBER MATRIX ADHESION; LAYERED STRUCTURE;

FIBER REINFORCED METALS;

COMPOSITE PROPERTIES; COMPOSITES, CARBON-FIBRE-REINFORCED; FIBRE/MATRIX ADHESION; FIBRE/MATRIX INTERFACE;

EID: 0031392909     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0266-3538(97)00108-5     Document Type: Article

References (24)

1. Marissen, R., Fatigue mechanisms in ARALL, a fatigue resistant hybrid aluminium aramid composite material. Fatigue 87, 1987, 3, 1271.
2. Marissen, R., Flight simulation behavior of aramid reinforced aluminum laminates (ARALL). Eng. Fract. Mech., 1984, 19(2), 261.
3. Marissen, R., Fatigue crack growth predictions in aramid reinforced aluminum laminates (ARALL). J. Aircraft, 1988, 25(2), 35.
4. Salivar, G. C. and Gardini, C. A., The influence of stress ratio and temperature on the fatigue crack growth rate behavior of ARALL®. J. Compos. Technol. Res., 1993, 15(1), 46.
5. Schijve, J., Fatigue of aircraft materials and structure. Fatigue, 1994, 16(1), 21.
6. Young, J. B., Landry, J. G. N. and Cavoulacos, V. N., Crack growth and residual strength characteristics of two grades of glass-reinforced aluminum 'GLARE'. Compos. Struct., 1994, 27, 457.
7. Vermeeren, C. A. J. R., The blunt notch behavior of metal laminates: ARALL and GLARE. TU Delft Report LR-617, Department of Aerospace Engineering, Delft University of Technology, The Netherlands, 1990.
8. th European Conf. on Fracture, Torino, Italy. Chameleon Press Ltd, London, 1990.
9. Macheret, J. and Bucci, R. J., A crack growth resistance curve approach to fiber/metal laminate fracture toughness evaluation. Eng. Fract. Mech., 1993, 45(6), 729.
10. Lawcock, G. D., Ye, L. and Mai, Y.-W., Progressive damage and residual strength of a carbon fibre reinforced metal laminate. J. Compos. Mater., 1997, 31, 762.
11. Lawcock, G. D., Ye, L., Sun, C.-T. and Mai, Y.-W., The effect of adhesive bonding between aluminium and composite prepreg on the mechanical properties of carbon fibre reinforced metal laminates. Compos. Sci. Technol., 1997, 57, 34.
12. Bucci, R. J. and Macheret, Y., Size effects in aluminium laminate notch strength determinations. In Proc. of Advanced Aerospace Materials/Processes Conf. and Exposition, Long Beach, California, 1991.
13. Kim, J. K. and Mai, Y.-W., Effects of interfacial coating and temperature on the fracture behaviours of unidirectional Kevlar and carbon fibre reinforced epoxy composites. J. Mater. Sci., 1991, 26, 4702.
14. Atkins, A. G., Intermittent bonding for high toughness/high strength composites. J. Mater. Sci., 1975, 10, 819.
15. Hibbs, M. F., Tse, M. K. and Bradley, W. L., Interlaminar fracture toughness and real time fracture mechanics of some toughened graphite/epoxy composites. In Toughened Composites, ASTM STP 937, ed. N. J. Johnston. American Society for Testing and Materials, Philadelphia, Pennsylvania, 1987, p. 115.
16. Hancox, N. L., Fibre Composite Hybrid Materials. Applied Science Publishers, London, 1981.
17. Cook, J. and Gordon, J. E., A mechanism for the control of crack propagation in all-brittle systems. Proc. Roy. Soc. London, 1964, A282, 508.
18. Baillie, C. A. and Bader, M. G., Some aspects of interface adhesion of electrolytically oxidised carbon fibres in an epoxy-resin matrix. J. Mater. Sci., 1994, 29, 3822.
19. Drzal, L. T., Rich, M. J. and Lloyd, P. F., Adhesion of graphite fibers to epoxy matrices: I. The role of fiber surface treatment. J. Adhesion, 1982, 16, 1.
20. Wegman, R. F., Surface Preparation Techniques for Adhesive Bonding. Noyes Publications, Park Ridge, New Jersey, 1989.
21. Standard test method for apparent interlaminar shear strength of parallel fiber composites by short-beam method, ASTM D 2344-84. American Society for Testing and Materials, Philadelphia, Pennsylvania, 1984.
22. Mattousch, A. C., Test procedures for fiber metal laminates. Report TD-R-93-003, Structural Laminates Company, Delft, The Netherlands, 1993.
23. Bateman, J. H., Hunt, M. O. and Sun, C. T., New interlaminar shear test for structural wood composites. Forest Products J., 1990, 40(30), 9.
24. th Tech. Conf., Technomic Pub. Co., Lancaster, PA, 1991, p. 732.