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← TechnologyWhich 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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