Size effect on compressive strength of T300/924C carbon fibre-epoxy laminates

Plastics, Rubber and Composites

Volumn 31, Issue 8, 2002, Pages 364-370

  Soutis, C ^a   Lee, J ^a   Kong, C ^b  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b Chosun University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; CARBON FIBERS; COMPRESSIVE STRENGTH; DELAMINATION; FRACTURE TOUGHNESS; LOADS (FORCES); STRESS ANALYSIS; X RAY RADIOGRAPHY;

CARBON FIBER-EPOXY LAMINATES;

PLASTIC LAMINATES;

EID: 0036943878     PISSN: 14658011     EISSN: None     Source Type: Journal    
DOI: 10.1179/146580102225006459     Document Type: Article

References (24)

1. C. ZWEBEN: Composites, 1994, 25, (6), 451-454.
2. C. ZWEBEN, W. S. SMITH, and M. W. WARDLE: Proc. 5th Conf. on 'Composite materials: testing and design', ASTM STP674, 1979, Pa, USA, American Society for Testing and Materials, pp. 228-262.
3. H. W. HERRING: 'Selected mechanical and physical properties of boron filaments', NASA report TN D-3202, 1966.
4. R. E. BULLOCK: J. Compos. Mater., 1974, 8, 200-206.
5. K. R. BERG and J. RAMSEY: 'Metal aircraft structural elements reinforced with graphite filamentary composites', NASA report CR-112162, 1972.
6. M. R. WISNOM: Compos. Struct., 1991, 18, 47-63.
7. M. E. WADDOUPS, J. R. EISENMANN, and B. E. KAMINSKI: J. Compos. Mater., 1971, 5, 446-454.
8. J. A. LAVOIE, C. SOUTIS, and J. MORTON: Compos. Sci. Technol., 2000, 60, 283-299.
9. C. P. MACKINLEY: 'Compressive failure of CFRP laminates containing pin-loaded holes', PhD thesis, Imperial College of Science, Technology and Medicine, 2000.
10. Airbus Industry Test Method: AITM-1.0008, Issue 2, June 1994.
11. Airbus Industry Test Method: 'Determination of in-plane shear properties (± 450 tensile test)' AITM 1.0002, June 1994.
12. J. G. HABERLE: 'Strength and failure mechanics of unidirectional carbon fibre-reinforced plastics under axial compression', PhD thesis, University of London, 1991.
13. C. SOUTIS: 'Compressive failure of notched carbon fibreepoxy panels', PhD thesis, University of Cambridge, 1989.
14. S. DRAPIER, C. GARDIN, J. GRANDIDIER, and M. POTIER-FERRY: Compos. Sci. Technol., 1996, 56, 861-867.
15. D. C. LAGOUDAS and A. M. SALEH: J. Reinf. Plast. Compos., 1993, 12, 1016-1023
16. M. M. MIKULAS: 'Failure prediction techniques for compression loaded composite laminate with holes', NASA report CP-2142, 1980.
17. M. D. RHODES, M. M. MIKULAS, and P. E. McGOWAN: AIAA J., 1984, 22, (9), 1283-1292.
18. D. HITCHINGS: 'FE77 users' manual'; 1995, London, Imperial College, Department of Aeronautics.
19. G. N. SAVIN: 'Stress concentration around holes'; 1961, Oxford, Pergamon Press.
20. C. SOUTIS, N. A. FLECK, and P. A. SMITH: J. Compos. Mater., 1991, 25, 1476-1498.
21. C. SOUTIS and P. T. CURTIS: Composites A, 2000, 31, 733-740.
22. C. SOUTIS, F. C. SMITH, and F. L. MATTHEWS: Composites A, 2000, 31, 531-536.
23. E. T. COMPONECHI, J. W. GILLESPIE, and D. J. WILKINS: J. Compos. Mater., 1993, 27, 471-490.
24. I. M. DANIEL and H. M. HSIAO: Int. J. Fract., 1999, 95, 143-158.