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Which outcome occurs when jet engine intake airflow exceeds Mach number limits?

A)Compressor stall leads to flow breakdown
B)Increased fuel efficiency becomes achievable
C)Engine thrust exponentially increases instead
D)Overall engine vibration amplitude decreases

💡 Explanation

Compressor stall occurs because exceeding the Mach number limit initiates a shockwave formation, leading to boundary layer separation and flow disruption initiating Dynamic stall. Therefore, compressor stall initiates flow breakdown, rather than improved efficiency which demands smooth airflow.

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