Fig. 12. (a) Residual flexural strength after cyclic thermal shock at 1500℃ [200]. (b) The cross-section morphology of the ((AlCrNbTa)2Ti)O2 coating [197]. (c) (WTaNbZrTi)C before and after the application of pressure t-ZrO2 and m-ZrO2 content changes, and the martensitic phase transition of ZrO2 under pressure schematic diagram, after the application of pressure the content of t-ZrO2 is significantly reduced, and the content of m-ZrO2 is increased accordingly [14]. (d) Comparison of the dependence of ideal tensile strength and nanoindentation hardness on VEC. The inset in A shows the geometric mean of the strain tensile strength recorded along [001] and [99] as a function of VEC [220]. (e) Mapping of nanohardness and elastic modulus in HEA50C [13].
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