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Which outcome contributes to separation when the Reynolds number increases past thresholds in airfoil design?

A)Increased laminar boundary layer attachment
B)Suppressed adverse pressure gradients
C)Amplified turbulent kinetic energy production
D)Reduced skin friction drag coefficient

💡 Explanation

Increased Reynolds number causes transition to turbulence; therefore, turbulent kinetic energy amplification develops because increased momentum transfer within the boundary layer enhances separation rather than delaying it as in laminar flow at lower Reynolds numbers.

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