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Which outcome occurs when subsonic airflow separates during flight?

A)Increased wave drag forms stall
B)Reduced skin friction lowers velocity
C)Pressure increases stabilize airflow
D)Laminar flow prevents induced drag

💡 Explanation

Increased wave drag leading to stall results because separation causes turbulent boundary layer at altitude during subsonic laminar flow disruption; therefore wave drag contributes to reduced lift rather than increased lift, because pressure stabilizes the stalled flow aloft.

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