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Which aerodynamic effect results in decreased lift during icing conditions?

A)Premature boundary layer separation
B)Increased static air pressure
C)Elevated induced drag coefficient
D)Enhanced laminar airflow adhesion

💡 Explanation

Icing on an aircraft wing disrupts smooth airflow which causes premature boundary layer separation; because of this separation, airflow detaches from the wing surface, therefore lift dramatically decreases rather than is enhanced or pressure rises.

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