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Which risk increases when turbine blades in a jet engine experience high vibratory stress?

A)Accelerated high cycle fatigue
B)Increased thermal barrier efficiency
C)Elevated compressor stall margin
D)Decreased fuel injection pressure

💡 Explanation

High vibratory stresses induce micro-cracks due to high cycle fatigue. Because the stress exceeds the material's endurance limit, cracks propagate rapidly; therefore failure occurs rather than slower, creep-related deformation under steady conditions.

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