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10 / CHAPTER 07

Boundary layers and separation

See how wall friction, adverse pressure gradients, and detachment arise.

Fluid Mechanics: original course diagram
A visual model for this course. Read it as a prompt for the assumptions behind the chapter.

ANCHOR EQUATION

Boundary-layer scale

δL∼Re−½

In symbols: δ/L ∼ Re⁻¹ᐟ²

Viscous effects organize into a thin boundary layer at high Reynolds number.

Poiseuille flow comes from a pressure–viscous balance

In a long, straight, circular pipe with steady laminar flow, pressure gradient drives the fluid while viscosity resists layer shear. The parabolic profile and strong radius dependence follow from integrating this balance.

Integrate the cylindrical momentum equation

For axial speed u(r), steady momentum gives 0 = −dp/dx + μ(1/r)d/dr(r du/dr). Integrate once: du/dr = (dp/dx)r/(2μ) after removing the singular center term. Integrate again and impose no-slip u(R)=0: u(r) = −(dp/dx)(R² − r²)/(4μ). Integrating Q = ∫₀^R 2πr u(r)dr yields Q = πR⁴Δp/(8μL).

For R = 1 mm, L = 1 m, Δp = 10 kPa, μ = 0.001 Pa·s, Q = π(10⁻³)⁴(10⁴)/(8×10⁻³) = 3.93×10⁻⁶ m³/s. Doubling R multiplies Q by 16.

Laminar is not automatic

The derivation assumes fully developed, steady, incompressible, Newtonian flow with no-slip and a circular tube. At high Re, turbulence changes the profile and pressure-drop law.

Work it: Use the formula to compare flow through 2 mm and 1 mm radius tubes at the same Δp and L. Explain why a partial blockage can have a dramatic effect.