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Which outcome characterizes a jet engine during surging?

A)Compressor stall and reversed airflow
B)Increased fuel 효율성 and combustion
C)Stable maximum thrust output achieved
D)Decreased turbine blade tip clearance

💡 Explanation

During surge, compressor stall causes reversed airflow due to insufficient pressure because some blades experience angles of attack above the critical level. Therefore, airflow becomes unsteady and reversed, rather than operating steadily; other options reflect normal, or optimized, turbine function.

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