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Which phenomenon explains increased drag at transonic speeds?

A)Adverse pressure gradient formation
B)Boundary layer flow separation
C)Shock wave-boundary layer interaction
D)Laminar-turbulent transition delay

💡 Explanation

Shock-induced separation occurs when a shockwave interacts with the boundary layer, causing flow reversal because the increased pressure decelerates airflow, and thus enhances turbulence intensity. Therefore option C is correct, rather than other transition or laminar effects.

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