The Darcy–Weisbach Equation

The Darcy–Weisbach equation gives the pressure lost to friction when fluid flows through a straight pipe: Δp = f·(L/D)·ρV²/2. Everything about the flow regime and the pipe wall is packed into the Darcy friction factor f, which is 64/Re for laminar flow and comes from the Colebrook equation or the Moody chart for turbulent flow.

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The equation

Friction loss grows with pipe length L, shrinks with diameter D, and scales with the dynamic pressure ρV²/2 of the flow. The Darcy friction factor f is the constant of proportionality: Δp = f·(L/D)·ρV²/2.

Dividing by ρg gives the head loss in metres of the flowing fluid, h_f = f·(L/D)·V²/(2g). Head is convenient for pumps, which are rated in head, and it does not depend on the fluid’s density.

Find the regime first with the Reynolds number. It decides which friction factor formula applies.

The friction factor

For laminar flow, f = 64/Re exactly, and the result is the Hagen–Poiseuille law. Wall roughness does not matter.

For turbulent flow, f depends on Re and the relative roughness ε/D. The Colebrook equation, 1/√f = −2·log10(ε/(3.7D) + 2.51/(Re·√f)), is implicit in f, so it is solved by iteration. The Moody chart is a plot of the same equation. Explicit fits such as Swamee–Jain give a close answer in one step and are a good starting guess.

The Darcy factor is four times the Fanning friction factor used in some chemical engineering texts. Check which one a chart or formula uses before you mix sources.

What the equation leaves out

Darcy–Weisbach covers straight, full pipe only. Valves, elbows, entrances and exits add minor losses, usually written as K·ρV²/2 per fitting, and elevation change adds ρgΔz. A pump must supply the sum. For compressible gases with a large pressure drop, density changes along the pipe and the line has to be split into short segments.

Key formulas

Formulas used on this page, with the textbook each is cited from
FormulaExpressionWhereCited from
Darcy–Weisbach equationΔp = f·(L/D)·ρ·V²/2f = Darcy friction factorWhite, Fluid Mechanics
Head lossh_f = Δp / (ρ·g) = f·(L/D)·V²/(2g)g = 9.81 m/s²Munson et al., Fundamentals of Fluid Mechanics
Laminar friction factorf = 64 / ReRe < about 2300White, Fluid Mechanics
Colebrook equation1/√f = −2·log10(ε/(3.7·D) + 2.51/(Re·√f))turbulent flow; solve by iterationColebrook (1939), Journal of the Institution of Civil Engineers
Swamee–Jain approximationf = 0.25 / [log10(ε/(3.7·D) + 5.74/Re^0.9)]²explicit fit to ColebrookSwamee & Jain (1976), Journal of the Hydraulics Division, ASCE

Worked examples

Example: Laminar pressure drop in a hydraulic line

Given

  • Oil flows at 6 L/min through 5 m of line with a 12 mm bore.
  • Take ρ = 870 kg/m³ and μ = 0.040 Pa·s, typical values for a mid-grade hydraulic oil at 40 °C.

Find

  • The Reynolds number and friction factor.
  • The pressure drop and head loss.

Solution

  1. Velocity, from Q = 1.0 × 10⁻⁴ m³/s and A = π × 0.012²/4.V = 1.0 × 10⁻⁴ / 1.131 × 10⁻⁴ = 0.884 m/s
  2. Reynolds number. It is far below 2300, so the flow is laminar.Re = 870 × 0.884 × 0.012 / 0.040 = 231
  3. Laminar friction factor.f = 64 / 231 = 0.277
  4. Darcy–Weisbach, with ρV²/2 = 870 × 0.884² / 2 = 340 Pa.Δp = 0.277 × (5 / 0.012) × 340 = 39 300 Pa = 39.3 kPa
  5. Check with Hagen–Poiseuille, which should agree exactly for laminar flow.Δp = 32·μ·L·V / D² = 32 × 0.040 × 5 × 0.884 / 0.012² = 39.3 kPa
  6. Head loss in metres of oil.h_f = 39 300 / (870 × 9.81) = 4.61 m

Answer: Re ≈ 231 (laminar), f ≈ 0.277, Δp ≈ 39.3 kPa and h_f ≈ 4.6 m of oil over the 5 m line.

Example: Turbulent head loss in a cooling-water line

Given

  • Water flows at 8 L/s through 120 m of steel pipe with an 80 mm bore.
  • Take ρ = 998 kg/m³ and μ = 1.0 × 10⁻³ Pa·s (typical for water near 20 °C) and ε = 0.045 mm, a value commonly used for new commercial steel.

Find

  • The friction factor.
  • The pressure drop and head loss.
  • How much the loss rises if the flow doubles.

Solution

  1. Velocity and Reynolds number. Re is far above 4000, so the flow is turbulent.V = 0.008 / (π × 0.08²/4) = 1.59 m/s, Re = 998 × 1.59 × 0.08 / 0.001 = 127 000
  2. Relative roughness, and a first estimate from Swamee–Jain.ε/D = 0.045 / 80 = 0.000563, f₀ = 0.25 / [log10(0.000563/3.7 + 5.74/127 000^0.9)]² = 0.0201
  3. Iterate Colebrook from f₀. It settles in two or three passes.1/√f = −2·log10(0.000563/3.7 + 2.51/(127 000·√f)) → f = 0.0200
  4. Darcy–Weisbach, with ρV²/2 = 998 × 1.59² / 2 = 1264 Pa.Δp = 0.0200 × (120 / 0.08) × 1264 = 37 900 Pa = 37.9 kPa
  5. Head loss.h_f = 37 900 / (998 × 9.81) = 3.88 m
  6. At 16 L/s, V doubles and Re = 254 000. Colebrook gives f = 0.0188, so the loss rises by less than four times.Δp = 0.0188 × 1500 × 998 × 3.18² / 2 = 142 kPa, a ratio of 3.75

Answer: f ≈ 0.0200, Δp ≈ 37.9 kPa and h_f ≈ 3.9 m. Doubling the flow raises the loss about 3.75 times, slightly less than V² because f falls as Re rises.

Common mistakes

In industry

Frequently asked questions

What is the difference between Darcy–Weisbach and Hazen–Williams?

Hazen–Williams is an empirical formula for water at ordinary temperatures. Darcy–Weisbach is dimensionally consistent and works for any Newtonian fluid, regime and pipe, which is why most fluid mechanics texts prefer it.

Why does Colebrook need iteration?

f appears on both sides of the equation, inside a logarithm, so there is no closed-form solution. A few rounds of substitution converge quickly, and explicit fits like Swamee–Jain give a close first guess.

Does roughness matter in laminar flow?

No. In laminar flow f = 64/Re regardless of the wall. Roughness starts to matter as the flow becomes turbulent and, at high Re, dominates.

Is there a calculator for this?

Yes. Coplain’s pipe pressure drop calculator, linked below, solves Colebrook and shows each step in SI or US units.

Keep learning

All Fluid Mechanics lessons · All engineering subjects

See also

Sources

  1. F. M. White, Fluid Mechanics, McGraw Hill
  2. B. R. Munson, T. H. Okiishi, W. W. Huebsch, A. P. Rothmayer, Fundamentals of Fluid Mechanics, Wiley
  3. C. F. Colebrook, Turbulent flow in pipes, with particular reference to the transition region between the smooth and rough pipe laws (1939), Journal of the Institution of Civil Engineers
  4. P. K. Swamee, A. K. Jain, Explicit equations for pipe-flow problems (1976), Journal of the Hydraulics Division, ASCE
  5. L. F. Moody, Friction factors for pipe flow (1944), Transactions of the ASME

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