Skip to main content
Log in

Strength of fiber reinforced metal laminates with a circular hole

  • Published:
Metals and Materials International Aims and scope Submit manuscript

Abstract

The effect of notching on fiber-reinforced metal laminates (FML) is studied 3-2 lay up carbon fiber aluminum laminates specimens containing a circular hole were employed in notch tests. The notch effect for a composite laminate was investigated and compared with carbon/epoxy composites and aluminum sheets. The degradation of notch strength for carbon fiber aluminum laminates was smaller than for carbon/epoxy composites. The point and average stress criteria were used in the notch strength analysis. A finite width correction factor was also used. The strength degradation models involve a single parameter that is a function of the hole size and the characteristic length. These models were compared with experimental data and good agreement was found.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. B. Z. Jang,Advanced Polymer composites: Principles and Applications, ASM International (1994).

  2. L. B. Vogelesang, J. W. Gunnink, G. H. Poebroeks, and R. P. G. Muller,Proc. 18 th Symposium of the International Committee on Aeronautical Fatigue (eds., J. M. Grandage and G. S. Jost), p. 257, EMAS, Warley, West Midlands, UK (1995).

    Google Scholar 

  3. A. N. Gribkow,Metal Matrix Composites (eds., J. N. Fridlyander), p. 487, Chapman & Hall, London (1995).

    Google Scholar 

  4. M. E. Waddoups, J. R. Eisenmann, and B. E. Kaminski,J. Compos. Mater. 5, 446 (1971).

    Article  CAS  Google Scholar 

  5. J. M. Whitney, and R. J. Nuismer,J. Compos. Mater. 8, 253 (1974).

    Article  Google Scholar 

  6. R. J. Nuismer, and J. M. Whitney,Uniaxial Failure of Composite Laminates Containing Stress Concentrations, In Fracture Mechanics of Composites: ASTM STP 593, p. 117, ASTM International (1975).

  7. B. D. Agarwal and L. J. Broutman,Analysis and Performance of Fiber Composites, 2 nd ed., John Wiley & Sons, New York (1990).

    Google Scholar 

  8. S. C. Tan,J. Compos. Mater. 22, 1080 (1988).

    Article  Google Scholar 

  9. J. Mar,Mechanics of Composite Review: Air-Force Material Laboratory and Air-Force Office of Scientific Research Technical Report, p. 117 (1976).

  10. R. B. Pipes, R. C. Wetherhold, and J. W. Gillespie, Jr.,J. Compos. Mater. 13, 148 (1979).

    Article  CAS  Google Scholar 

  11. H. K. Kim, W. Hwang, and K. S. Han,Sci. Eng. Compos. Mater. 3, 11 (1994).

    Google Scholar 

  12. R. F. Wegman,Surface Preparation Techniques for Adhesive Bonding, Noyes Publications, NJ (1989).

    Google Scholar 

  13. G. D. Lawcock, L. Ye, Y. W. Mai, and C. T. Sun,Compos. Sci. Technol. 57, 1609 (1997).

    Article  CAS  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to W. Hwang.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Hwang, W.J., Park, Y.T. & Hwang, W. Strength of fiber reinforced metal laminates with a circular hole. Met. Mater. Int. 11, 197–204 (2005). https://doi.org/10.1007/BF03027442

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF03027442

Keywords

Navigation