“…In turn, La and Ce have negligible solid solubility in an α-Mg matrix Ce form the layers of intermetallic phases, which completely wet the Mg/Mg G Figure 21). GB wetting by the intermetallic Mg-RE phases was also observed in M 4Zn [126], Mg-5Sn-2Zn-0.5Zr (wt%) [128], Mg-2Dy-0.5Zn (wt%) [129], Mg-14L alloys [130] and AZ31/ZK60 bimetal rods [131]. GB wetting by a second solid phase was observed in multicomponent highalloys (HEA) such as in arc-melted CoFeNi0.5AlCrx (x = 0.25, 0.50, 0.75 and 1.00) all treated at 1200 °C [84], CoCrFeNi(SiC)x alloy deposited powder plasma arc additiv ufacturing [132], in Al0.2MoNbTaTiW/MC refractory HEA composite manufactu spark plasma sintering and hot extrusion [134], carbon-alloyed FeMnCr-NiCo0.95C subjected to different thermal-mechanical treatments [136], AlCoCrFeNiTi-C H GB wetting by a second solid phase was observed in multicomponent high-entropy alloys (HEA) such as in arc-melted CoFeNi 0.5 AlCr x (x = 0.25, 0.50, 0.75 and 1.00) alloy heat treated at 1200 • C [84], CoCrFeNi(SiC) x alloy deposited powder plasma arc additive manufacturing [132], in Al 0.2 MoNbTaTiW/MC refractory HEA composite manufactured by spark plasma sintering and hot extrusion [134], carbon-alloyed FeMnCr-NiCo 0.95 C 0.05 HEA subjected to different thermal-mechanical treatments [136], AlCoCrFeNiTi-C HEA annealed at 1200 • C [138], NiCoCrAlY coating on 304 stainless steel laser processed at 950 • C [139], spark plasma sintered (SPS) HfNbTaTiZr HEA [140], AlCoCrCuFeNi HEA heat treated at 1200 • C [141], AlCoCrFeNiCu HEA coating deposited by the high velocity oxygen fuel spraying (HVOF) and vacuum heat treatment (VHT) at different temperatures (500, 700, 900 and 1100 • C) [142], AlNb 2 TiV low-weight refractory HEA [143] ans Al 10 Co 19 Cr 16 Fe 20 Ni 35 HEA homogenized at 1200 • C and annealed at 800 • C and at 590 • C [144].…”