Design of binder jet additive manufactured co-continuous ceramic-reinforced metal matrix composites
Pablo D. Enrique*(), Ehsan Marzbanrad, Yahya Mahmoodkhani, Ali Keshavarzkermani, Hashem Al Momani, Ehsan Toyserkani, Norman Y. Zhou

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Fig. 9.. Maximum Cr3C2 shell volume fraction achievable with varying Cr concentrations in the starting powder. Values for some Ni-based alloys and the current study’s MMC are shown, with adjustments (no-fill shapes) for Mo solubility in the Cr3C2 shell.