Engine Gas Turbines (Supplementary) USCG Question #19 (Set 1)

Each stage of an axial-compressor of a gas turbine can compress the atmospheric air a total of how many times?

Official USCG Answer & Rule Citation

Correct Answer: Option C — 1.2 times

Axial-flow compressor stages are designed for high efficiency with relatively low pressure ratios per stage. Typically, each stage achieves a pressure ratio of approximately 1.2:1. This incremental compression allows for a multi-stage design that avoids excessive air heating and aerodynamic stalling within the compressor.

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