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← TechnologyWhich phenomenon decreases landing lift on an aircraft?
A)Increased flow streamline separation earlier✓
B)Higher angle of attack effectiveness
C)Lower parasitic drag coefficient increase
D)Elevated Reynolds number similarity achieved
💡 Explanation
Flow streamline separation on a wing causes a stall, decreasing lift coefficient because the boundary layer detaches. This separation weakens lift rather than increasing it, therefore stall is hazardous near landing rather than optimal airflow.
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