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← ScienceWhich 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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