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Which limitation develops in aircraft design when exceeding critical airspeeds?

A)Unsteady lift due to flow separation
B)Elevated skin friction drag
C)Increased engine combustion instability
D)Control surface icing inefficiencies

💡 Explanation

Exceeding an aircraft's critical airspeed precipitates flow separation and turbulent wake formation which leads to unsteady lift, because exceeding the critical speed increases the Reynolds number, fostering turbulence. Subsequently pilots face reduced control authority; therefore the correct option is flow separation rather than increased drag or instability under normal conditions.

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