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JAA ATPL Question 4894
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JAA ATPL Question 4894
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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decrease the intensity of shock wave induced air separation.
decrease the span wise flow at high Mach Numbers.
increase the magnitude of the shock wave.
increase the critical Mach Number.
2,025 votes ยท 22 hours left
Vortex generators on the upper side of the wing surface will:
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