Test 10 Questions EASA PPL(A) - Private Pilot License - Principle of Flight, no time limit

1 - Which statement about the airflow around an aerofoil is correct if the angle of attack decreases?
2 - Which option states a benefit of wing washout?
3 - Point number 5 in the figure indicates which flight state? See figure (PFA-008)
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4 - When extending the flaps for landing at constant angle of attack, in which way does the lift coefficient change far before reaching the maximum lift coefficient?
5 - Compared to trailing edge flaps, leading edge devices like Slots...
6 - The laminar boundary layer on the aerofoil is located between...
7 - The right aileron deflects upwards, the left downwards. How does the aircraft react?
8 - In motorplanes the stall warning is usually activated by a change of...
9 - How is the balance of forces affected during a turn?
10 - How do lift and drag change when setting flaps to a lower position?