“…(b) Corresponding strain-hardening response for the annealed TiZrNbTa HEAs. (c) Changing rate of yield strength versus that of elongation with the increase in annealing temperature for the introduced TiZrNbTa HEAs relative to other reported HEAs [6,[31][32][33][34][35][36][37][38][39], steels [3,[40][41][42][43][44], copper alloys[45][46][47][48], aluminum alloys [5,[49][50][51], titanium alloys [4,[52][53][54], magnesium alloys[55][56][57], pure metals[58][59][60], nickel alloys[61], molybdenum alloy[62], and zirconium alloy[63]. The properties of strength and ductility obtained after HTA and LTA are denoted as Y HTA and Y LTA , respectively.…”