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Which phenomenon limits jet engine efficiency at higher compression ratios?

A)Increased fuel burn rates faster
B)Accelerated compressor blade stall speed
C)Exceeding the compressor surge line
D)Decreased turbine blade temperature limits

💡 Explanation

Exceeding the compressor surge line occurs because of increased pressure differentials destabilizing airflow in the compressor during the Brayton cycle; therefore airflow reverses creating surge, rather than efficient compression because pressure rises past stability threshold.

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