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Which outcome occurs when a supersonic aircraft experiences a sudden, uncommanded aileron reversal at high dynamic pressure?

A)Reduced roll control effectiveness
B)Increased structural skin friction
C)Enhanced boundary layer adhesion
D)Stabilized lateral oscillatory damping

💡 Explanation

Reduced aerodynamic forces cause aileron reversal because torsional deformation exceeds control input via aeroelasticity, therefore diminishing roll control, rather than enhancing stability; this happens due to increased loads and material limitations within aircraft systems.

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