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Which outcome arises during high-speed flight surpassing design constraints?

A)Onset of transonic flow instability
B)Increased structural fatigue resistance
C)Reduced aerodynamic drag coefficient values
D)Enhanced laminar boundary layer attachment

💡 Explanation

Transonic flow instability appears because exceeding designed flight speed triggers *compressible flow effects*, invalidating incompressible Bernoulli assumptions; therefore shockwaves form, rather than drag reduction, because energy dissipates into turbulent eddies instead.

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