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Which consequence results when the Reynolds number significantly increases within an aircraft's hydraulic control system?

A)Increased laminar flow stability margins
B)Decreased pressure drop across valves
C)Onset of turbulent flow regime
D)Enhanced lubrication of system components

💡 Explanation

Increased Reynolds number signifies inertial forces dominate viscous forces, leading to the onset of turbulent flow because instabilities grow faster; therefore, turbulence ensues, rather than laminar flow becoming more stable because increased viscosity dampens disturbances.

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