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JAA ATPL Question 4896
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JAA ATPL Question 4896
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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decrease the stalling speed by increase of the tangential velocity of the swept wing.
decrease the interference drag of the trailing edge flaps.
decrease the shock wave induced separation.
increase the effectiveness of the spoiler due to increase in parasite drag.
2,025 votes ยท 22 hours left
Vortex generators mounted on the upper wing surface will
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