A simple analysis of the hot consolidation of metal-matrix composite panels from tapecast monotape layups

摘要

Continuous-fiber, metal-matrix composites (MMCs) offer great promise as advanced aerospace materials for high-temperature applications. For example, MMCs with titanium alloy matrices provide an excellent combination of high-temperature strength, creep resistance, stiffness, and lightweight [1]. Nevertheless, critical issues related to cost and manufacture pose a major challenge to the implementation of these materials.