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Which immediate consequence results from airflow separation across an aircraft wing?

A)Drastic stall and lift reduction
B)Increased turbulent kinetic energy aloft
C)Elevated skin friction drag profile
D)Improved boundary layer laminar flow

💡 Explanation

Flow separation prevents the wing from generating lift; this causes a stall because the boundary layer detaches from the wing's surface, dramatically reducing lift and increasing drag; rather than streamlined flight, catastrophic descent ensues.

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