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Aerospace Engineering
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Aerodynamics
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Laminar Flow Regime
Laminar Flow Regime
A flow regime characterized by smooth, orderly fluid motion where viscous forces dominate. The shear stress is linearly proportional to the velocity gradient,
τ
=
μ
∂
u
∂
y
\tau = \mu \frac{\partial u}{\partial y}
τ
=
μ
∂
y
∂
u
. This typically occurs at low Reynolds numbers.