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Which outcome increases when fluid flow exceeds Reynolds number constraints within an aircraft's fuel line?

A)Increased static pressure recovery
B)Reduced boundary layer separation
C)Transition to turbulent flow
D)Greater laminar sublayer thickness

💡 Explanation

Exceeding the Reynolds number threshold prompts a laminar to turbulence transition because the inertial forces dominate viscous forces initiating small perturbations which grow exponentially due to momentum transfer, therefore causing turbulent flow, rather than orderly flow, impacting delivery.

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