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← ScienceWhich outcome occurs when helicopter rotor tip speed increases?
A)Compressibility effects reduce lift efficiency✓
B)Induced drag abruptly increases airflow
C)Vortex shedding stabilizes airfoil performance
D)Boundary layer remains laminar consistently
💡 Explanation
Compressibility effects arise because exceeding the critical Mach number initiates turbulence, thereby increasing drag. This reduces lift efficiency because shock waves rather than smooth flow develop around the rotor tip, therefore select A rather than option B which is about 'induced drag'.
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