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Which outcome occurs when the boundary layer transitions from laminar to turbulent flow across an aircraft wing, based on the momentum equation?

A)Increased skin friction drag
B)Reduced pressure gradient effects
C)Delayed flow separation point
D)Decreased lift-to-drag ratio

💡 Explanation

Increased skin friction drag occurs because transitioning to turbulence causes increased mixing and momentum transfer near the surface; therefore the drag increases rather than decreasing lift because laminar flow minimizes friction, and delayed separation involves pressure gradients.

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