Module 15 Gas Turbine Engine Practice Questions - UK CAA Part-66 AME Module 15 - Gas Turbine Engine Exam

What is the primary function of a convergent subsonic engine inlet duct?

Increase air velocity and decrease static pressure before entering the compressor Decrease air velocity and increase static pressure before entering the compressor Maintain supersonic airflow velocity up to the first stage compressor rotor Mix bypass air with primary combustion core air

Correct Answer:

Decrease air velocity and increase static pressure before entering the compressor

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