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2. Ni superalloys are the choice for mechanical structures in space applications at 650-1,100°C because they provide both hig
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Solution- As the tempevature is incread the stvength af moet decTeased bu ftom thema acbatiomakes it easie fodislocations to1 Thus, the Strength onty decneasuft 6ooc , whethes the -Uheima civatiodently violent which allows dislaaation inode to oves

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    uperalloys are the choice for mechanical structures in space applications at 650-1,100°C because they provide both high strength and good oxidation/corrosion resistance. For the majority of engineering materials, such as Fe, Cu, Al and Ti alloys, their yield strength decreases rapidly with increasing temperature, as shown in Figure 1(a). Nevertheless, the yield strength of Ni superalloys increases with increasing temperature until close to the alloys' melting point, as shown in Figure 1(b) Please explain why they behave so uniquely? (25...

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