journal article·1996-04

Computational Simulation of Matrix Microslip Bands in SiC/Ti-15 Composite

S. K. Mital, H. -J. Lee, P. L. N. Murthy, C. C. Chamis

Publisher page

Abstract

Computational simulation procedures are used to identify the key deformation mechanisms for a [0]8 and a [90]8 SiC/Ti-15 metal matrix composite. The computational simulation procedures employed consist of a three-dimensional finite-element analysis and a micromechanics-based computer code METCAN. The interphase properties used in the analysis have been calibrated using the METCAN computer code with the [90]8 experimental stress-strain curve. Results of the simulation show that although shear stresses are sufficiently high to cause the formation of some slip bands in the matrix concentrated mostly near the fibers, the nonlinearity in the composite stress-strain curve in the case of the [9018 composite is dominated by interfacial damage, such as microcracks and debonding rather than microplasticity. The stress-strain curve for the [0]8 composite is largely controlled by the fibers and shows only slight nonlinearity at higher strain levels that could be the result of matrix microplasticity.
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Research context

OpenAlex topics: Advanced ceramic materials synthesis · Aluminum Alloys Composites Properties · Advanced Surface Polishing Techniques

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

University of Toledo, Toledo, OH 43606

National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135

References (10)

Show source-provided references
1. Chamis, C. C. · 1990
2. Lee, H.-J. · 1991
3. Lee, H.-J. · 1991
4. Lerch, B. A. · 1989
5. Lerch, B. A. · 109
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9. 10.1016/0045-7949(90)90395-I10.1016/0045-7949(90)90395-I ↗
10. Newaz, G. M. · 1991 · 55