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Which risk escalates after an airfoil exceeding stall angle?

A)Increased boundary layer flow turbulence
B)Decreased adverse pressure gradients
C)Minimized flow separation laminarization
D)Optimal boundary layer energy recovery

💡 Explanation

Increased turbulence arises because flow separation prompts vortices, therefore escalating parasitic drag, rather than decreasing pressure gradients or enhancing laminarization; boundary layer turbulence then intensifies.

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