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Which consequence results when transonic airflow encounters adverse pressure gradients?

A)Boundary layer flow reversal occurs
B)Lift-induced drag substantially decreases
C)Laminar flow definitively transitions
D)Aerodynamic heating uniformly reduces

💡 Explanation

Flow reversal occurs because separation becomes dominant due to increased adverse pressure, triggering turbulent flow, increasing momentum near the wall through the mechanism of momentum diffusion; therefore, separation will occur, rather than improved aerodynamic heating because compressibility effects dominate.

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