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186 - ATPL Question Bank in English - For a conventional aerofoil with a simple hinged plain trailing-edge flap, neglect compressibility and wing-area change. When the flap is extended while steady level flight at the same mass and IAS is maintained by reducing angle of attack:

Question 186 - Principles of Flight - ATPL - Airline Transport Pilot Licence

The lift coefficient and the drag coefficient increase
The stall speed increases
The centre of pressure moves aft
The total boundary layer becomes laminar

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