TECHNICAL PAPERS
Jan 1, 1993

Improved Method for Determining Interfacial Stresses in Composites

Publication: Journal of Aerospace Engineering
Volume 6, Issue 1

Abstract

The conventional finite element method shows its weakness in determining the stress distributions along fiber matrix interfaces. This is because the chosen element displacement functions do not explicitly and/or implicitly satisfy the equilibrium and compatibility conditions that prevail at the interfaces. A procedure has been proposed to modify the conventional finite element method so as to allow the elastic stresses along the fiber matrix interfaces of two‐ and three‐dimensional fiber‐reinforced composites to be determined with improved accuracy. The results obtained by this modified method for a two‐dimensional problem are compared with both a photoelastic and a traditional finite elelment solution. The comparison shows that the modified solution is in better agreement with the photoelastic test data than the traditional solution. The results obtained by the modified method for a three‐dimensional problem are compared with a traditional finite element solution and the modified method is found to be superior.

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References

1.
Allison, I. M., and Hollaway, L. C. (1967). “Stresses in fibre reinforced materials.” British J. of Appl. Physics, London, England, 18, 979–989.
2.
Bathe, K. J. (1982). “Formulation and calculation of isoparametric finite element matrices,” Finite element procedures in engineering analysis, Prentice‐Hall, Englewood Cliffs, N.J., 194–300.
3.
Soh, A. K. (1985). “On the determination of interfacial stresses in a composite material.” J. of the British Society of Strain Measurement, 21(4), London, England, 163–172.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 6Issue 1January 1993
Pages: 90 - 103

History

Received: Dec 17, 1990
Published online: Jan 1, 1993
Published in print: Jan 1993

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Ai‐Kah Soh
Assoc. Prof., School of Mech. and Prod. Engrg., Nanyang Tech. Univ., Nanyang Ave., Singapore 2263

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