Hostname: page-component-cd9895bd7-jkksz Total loading time: 0 Render date: 2024-12-25T07:06:45.241Z Has data issue: false hasContentIssue false
  • English
  • Français

Through thickness fatigue failure of fibre-reinforced composites

Published online by Cambridge University Press:  04 July 2016

M. R. Wisnom  and
M. I. Jones
M. R. Wisnom
Affiliation:
Department of Aerospace Engineering University of Bristol Bristol, UK
M. I. Jones
Affiliation:
Department of Aerospace Engineering University of Bristol Bristol, UK
Get access Rights & Permissions [Opens in a new window]

Abstract

Simple straight and curved beams of unidirectional glass-epoxy were tested in fatigue to investigate failure under overall interlaminar tension and shear combined with local stresses at cut plies. Similar behaviour was observed as under static loading, with overall and local stresses interacting to cause delamination. When normalised, all the results lay close to, or above, a line determined from previous tension tests on specimens with cut plies, suggesting that this could be used as the basis for through thickness fatigue strength calculations.

Type
Research Article
Information
The Aeronautical Journal , Volume 102 , Issue 1012 , February 1998 , pp. 83 - 88
Copyright
Copyright © Royal Aeronautical Society 1998 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Hiel, C.C., Sumich, M. and Chappell, D.P. A curved beam test specimen for determining the interlaminar tensile strength of a laminated composite, J Comp Mat, 1991, 25:854-81.Google Scholar
2. Martin, R.H. and Jackson, W.C. Damage prediction in cross-plied curved composite laminates, NASA TM 104089, 1991.Google Scholar
3. Murri, G.M., Salpekar, S.A. and O'Brien, T.K., Fatigue delamination onset prediction in unidirectional tapered laminates, Comp Mat: Fatigue and Fracture, ASTM STP 1110, 1991, 3, pp 312–339.Google Scholar
4. Wisnom, M.R., Jones, M.I. and Cui, W. Delamination in composites with terminating internal plies under tension fatigue loading, Comp Mat: Fatigue and Fracture, ASTM STP 1230, 1995, 5, pp 486–508.Google Scholar
5. Wisnom, M.R., Jones, M.I. and Cui, W. Delamination of unidirectional glass fibre-epoxy with terminating plies under compression fatigue loading, Fibre Reinforced Composites, 1994, Newcastle, March 1994, pp 2/1-9.Google Scholar
6. Wisnom, M.R., Jones, M.I. and Cui, W. Failure of tapered composites under static and fatigue tension loading, AIAA J, 1995, 33, pp 911–918.Google Scholar
7. Wisnom, M.R. and Jones, M.I. Delamination due to interaction between overall interlaminar shear and stresses at terminating plies, Comp Struct, 1995, 31, pp 39–47.Google Scholar
8. Wisnom, M.R. and Jones, M.I. Delamination due to interaction between curvature induced interlaminar tension and stresses at terminating plies, Comp Struct, 1995, 32, pp 615–620.Google Scholar
9. Wisnom, M.R. and Jones, M.I. Size effects in interlaminar tensile and shear strength of unidirectional glass fibre-epoxy, J Rein Plast and Comp, 1996, 15, pp 2–15.Google Scholar
10. Petrossian, Z., Wisnom, M.R. and Jones, M.I. Prediction of delamination growth at discontinuous plies due to cyclic loading, 4th int conference on deformation and fracture of Composites, UMIST, March 1997, pp 253-261.Google Scholar
11. Petrossian, Z. and Wisnom, M.R. Improved fracture mechanics predictions for delamination of composites accounting for yield zones, 11th int conference on composite materials, Gold Coast, Australia, July 1997.Google Scholar