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Which consequence results when rapid turbine shaft deceleration occurs?

A)Compressor stall initiates upstream airflow reversal
B)Turbine blade creep rate decreases gradually
C)Combustion chamber pressure remains stable
D)Fuel injector nozzles sustain uniform flow

💡 Explanation

Compressor stall can occur following rapid deceleration due to a surge where pressure builds and airflow begins moving backwards, rather than smoothly onward, because decreased shaft speed lowers momentum; therefore, the incoming momentum opposes forward flow; rather than other effects limited by flow disruptions.

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