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← TechnologyWhich 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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