NASA NTRS · 19910020967
Interphase layer optimization for metal matrix composites with fabrication considerations
Abstract
A methodology is presented to reduce the final matrix microstresses for metal matrix composites by concurrently optimizing the interphase characteristics and fabrication process. Application cases include interphase tailoring with and without fabrication considerations for two material systems, graphite/copper and silicon carbide/titanium. Results indicate that concurrent interphase/fabrication optimization produces significant reductions in the matrix residual stresses and strong coupling between interphase and fabrication tailoring. The interphase coefficient of thermal expansion and the fabrication consolidation pressure are the most important design parameters and must be concurrently optimized to further reduce the microstresses to more desirable magnitudes.
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Morel, M., Saravanos, D. A., Chamis, C. C.. 1991-01-01. Interphase layer optimization for metal matrix composites with fabrication considerations. https://ntrs.nasa.gov/citations/19910020967
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