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JAA ATPL Question 4693
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JAA ATPL Question 4693
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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The stagnation point is another name for centre of pressure.
As the angle of attack increases, the stagnation point on the wing's profile moves downwards.
The stagnation point is always situated on the chordline, the centre of pressure is not.
The centre of pressure is the point on the wing's leading edge where the airflow splits up.
2,025 votes ยท 22 hours left
Which statement is correct?
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