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Which consequence results when thermal gradients exceed creep limits in turbine disc alloys?

A)Decreased turbine blade resonance frequency
B)Accelerated fatigue crack propagation rate
C)Elevated compressor stall margin degradation
D)Reduced turbine exhaust gas temperature

💡 Explanation

Fatigue crack propagation accelerates when thermal gradients stress alloy grain boundaries. This occurs because vacancies coalesce via grain boundary diffusion during the **Nabarro–Herring creep** mechanism. Therefore accelerated crack growth occurs, rather than decreased resonance as grain size grows at a slower rate.

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