CAA NZ Basic Turbine Knowledge (Aeroplane) Practice Questions - CAA NZ Basic Turbine Knowledge (Aeroplane) Exam (New Zealand) Exam

What is the primary purpose of the diffuser section positioned downstream of the compressor?

To decrease air velocity and increase static pressure before combustion To increase air velocity and decrease static pressure before the turbine To mix fuel evenly with high-speed air prior to ignition To cool high-temperature air before it enters the turbine

Correct Answer:

To decrease air velocity and increase static pressure before combustion

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