Part-66 Module 11 Practice Questions - EASA Part-66 Module 11 - Aeroplane Aerodynamics, Structures And Systems Exam

A leading-edge slat improves the low-speed lift of a wing primarily by:

Increasing the wing camber only Reducing the wing area to lower stall speed Energising the boundary layer and delaying the stall to a higher angle of attack Increasing the chord line incidence relative to the fuselage

Correct Answer:

Energising the boundary layer and delaying the stall to a higher angle of attack

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