EASA ATPL 081 Principles Of Flight Practice Questions - EASA ATPL Theory - Principles Of Flight (081) Exam

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On a conventional cambered aerofoil at a small positive angle of attack, the chordwise point of lowest static pressure (suction peak) is normally located:

At the trailing edge Near the leading edge on the upper surface At the centre of pressure On the lower surface near mid-chord

Correct Answer:

Near the leading edge on the upper surface

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