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Which flow outcome results when Reynold's equation exceeds viscosity limits within an aircraft's microfluidic cooling system?

A)Laminar flow becomes non-linear
B)Poiseuille equation remains applicable
C)Stable flow self-correct spontaneously
D)Entrance length extends indefinitely

💡 Explanation

Turbulence increases due to inertial forces dominating viscosity, therefore non-linear flow arises rather than stable flow, because the transition depends on the Reynold's number, where energy dissipates chaotically from eddy formations.

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