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Home > Exam Questions > EASA PPL(A) - Private Pilot Licence (Aeroplane) > Principles of Flight (Aeroplane) > For a conventionally cambered aerofoil before stall and at positive lift coefficient, the centre of pressure generally...

21 - EASA PPL(A) Theory Exam Questions in English - For a conventionally cambered aerofoil before stall and at positive lift coefficient, the centre of pressure generally...

Question 21 - Principles of Flight (Aeroplane) - EASA PPL(A) - Private Pilot Licence (Aeroplane)

Moves to the leading edge while the angle of attack becomes smaller.

Is located at approximately 25% of the chord, measured from the leading edge.

Moves to the trailing edge while the angle of attack becomes smaller.

Does not move since it is independent of the angle of attack.

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