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JAA ATPL Question 4716
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JAA ATPL Question 4716
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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Tip vortices can be diminished by vortex generators.
The wing tip vortices and the induced drag decrease at increasing angle of attack.
The flow direction at the upper side of the wing has a component in wing root direction, the flow at the underside of the wing in wing tip direction.
The flow direction at the upper and under side of the wing, both deviate in wing tip direction.
2,025 votes ยท 22 hours left
Which statement about induced drag and tip vortices is correct?
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