Fig. 12. (a) Residual flexural strength after cyclic thermal shock at ${1500}^{\circ }\mathrm{C}$. Reproduced from Ref [200]. Copyright Elsevier 2024. (b) The cross-section morphology of the ((AlCrNbTa)2Ti)O2 coating. Reproduced from Ref [197]. Copyright Elsevier 2024. (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. Reproduced from Ref [14]. Copyright The Nature Publishing Group 2023. (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. Reproduced from Ref [99] Copyright Elsevier 2025. as a function of VEC. Reproduced from Ref [220]. Copyright American Association for the Advancement of Science 2023. (e) Mapping of nanohardness and elastic modulus in HEA50C. Reproduced from Ref [13]. Copyright Elsevier 2024.
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