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Which outcome occurs when jet engine inlet airflow separates?

A)Compressor stall initiates rapidly
B)Turbine blade cooling improves
C)Thrust specific fuel burns reduce
D)Exhaust gas temperature decreases

💡 Explanation

Compressor stall occurs because flow separation causes rotating blades to experience excessive angles of attack, which disrupts airflow. Therefore, stall initiates quickly, rather than improved cooling due to turbulent flow or reduced temperature from inefficient compression.

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