High-temperature materials and creep

A fine-grained polycrystalline metal was creep tested at a low stress at about 0.5 times its melting point (in absolute temperature). The steady-state creep rate was nearly proportional to stress (stress exponent n ≈ 1) and nearly inversely proportional to the cube of the grain size. Which creep mechanism is most likely to be operating?

  1. APower-law creep controlled by dislocation climb in the grain interiors
  2. BCoble creep by diffusion of atoms along grain boundaries
  3. CNabarro–Herring creep by lattice diffusion through the grain interiors
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Answer: B. Coble creep by diffusion of atoms along grain boundaries

In diffusion creep, atoms diffuse from grain boundaries under tension to those under compression, elongating the grains, and the rate is proportional to stress (n = 1). When the diffusion path runs along the grain boundaries it is called Coble creep, and the rate is inversely proportional to the cube of the grain size. When it is lattice diffusion through the grain interiors it is called Nabarro–Herring creep, and the rate is inversely proportional to the square of the grain size. Grain boundary diffusion has a lower activation energy than lattice diffusion, so Coble creep dominates at relatively low temperatures and fine grain sizes, while the contribution of Nabarro–Herring creep grows at high temperatures near the melting point. Power-law creep by dislocations has a large n of 3 to 8 and hardly depends on grain size.

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More High-temperature materials and creep questions

  1. Which statement about the deformation mechanism map of Ashby and coworkers (with stress normalized by the shear modulus, σ/G, on the vertical axis and homologous temperature T/Tm on the horizontal axis) is correct? Tm is the melting point in absolute temperature.
  2. At room temperature, refining the grains raises strength (the Hall–Petch relation), but components loaded for long times at high temperature often use coarse grains or single crystals. Which is the correct reason?
  3. A heat-resistant alloy ruptured by creep in 1000 h at 1000 K under a certain stress. Assuming the Larson–Miller parameter P = T(C + log₁₀t_r) (T is the absolute temperature, t_r is the rupture time in h, and C = 20) is constant at the same stress, which temperature is closest to that giving a rupture life of 10⁵ h at the same stress?
  4. Which statement about the γ' phase that provides the high-temperature strength of nickel-based superalloys is correct?
  5. Why are directionally solidified columnar-grained or single-crystal nickel-based superalloys used for jet engine turbine blades?