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JAA ATPL Question 4878
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JAA ATPL Question 4878
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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separation of the flow at high angles of attack and at high Mach Numbers.
separation of the flow behind the bow wave.
separation of the flow at the trailing edge of the wing at high Mach Numbers.
separation of the boundary layer behind the shock wave.
2,025 votes ยท 22 hours left
Shock stall is:
#atpl
#jaa
#dgca
#pilot
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