Module 14 Propulsion Practice Questions - UK CAA Part-66 AME Module 14 - Propulsion Exam

What is the primary function of a gas turbine engine inlet duct on a subsonic transport aircraft?

To increase air velocity and reduce static pressure before entering the compressor To convert kinetic energy of the incoming air into static pressure with minimal total pressure loss To mix bleed air with ambient air to prevent compressor stall To meter the mass airflow directly into the combustion chamber

Correct Answer:

To convert kinetic energy of the incoming air into static pressure with minimal total pressure loss

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