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Which turbine blade 'flutter' risk increases when exceeding material tensile limits?

A)Resonance frequency dramatically shifts lower
B)Creep deformation induces early failure
C)Thermal fatigue stress is lessened now
D)Compressor stall risk mysteriously declines

💡 Explanation

Exceeding turbine alloy tensile yield strength leads to plastic deformation and reduced stiffness; the aeroelastic resonance frequency dramatically shifts lower because stiffness relates intimately to flutter limits, therefore dangerous resonance-induced fluttering increases, rather than mitigates.

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