The Weber Number — Inertia vs. Surface Tension

“Why are raindrops spherical? Why does an inkjet droplet land precisely without spattering? Why does diesel fuel shatter into micron-scale droplets inside a combustion chamber? The Weber number governs all of these — it is the gatekeeper of every fluid interface.”

1. Introduction

In large-scale flows — rivers, ocean currents, pipe networks — surface tension is negligible and can safely be ignored. But whenever the characteristic length scale shrinks to millimetres or below, or whenever high-speed flow impinges on a fluid interface, surface tension becomes a dominant force. The Weber number (We) quantifies the competition between inertial forces, which tend to deform and break interfaces, and surface tension, which resists deformation and drives interfaces toward minimum-area (spherical) shapes.

The Weber number answers: Does flow have enough inertia to overcome surface tension and rupture the interface? Its value governs droplet formation, jet stability, bubble dynamics, spray atomisation, inkjet printing, and the sinking-funnel problem of IYPT 2027.

Definition and Parameters

$$We = rac{
ho v^2 L}{sigma}$$

  • $
    ho$ — fluid density (kg/m³)
  • $v$ — characteristic velocity (m/s)
  • $L$ — characteristic length: droplet/bubble diameter, jet radius, or nozzle diameter (m)
  • $sigma$ — surface tension coefficient (N/m)

Dimensional check: $[
ho v^2 L/sigma] = ( ext{kg/m}^3)( ext{m}^2/ ext{s}^2)( ext{m})/( ext{N/m}) = ext{Pa·m}/( ext{N/m}) = ext{dimensionless}$.

Alternatively: $We = F_{inertia}/F_{surface,tension} sim (
ho v^2 L^2)/(sigma L) =
ho v^2 L/sigma$.

2. Historical Note

Moritz Weber (1871–1951) was a German mechanical engineer and professor at the Technische Hochschule Berlin. In 1919 he systematised the theory of dynamic similarity for flows involving viscosity and surface tension, introducing what became known as the Weber number. Weber was motivated by the need to correctly scale model experiments of ship propellers and hydraulic machinery — situations where surface tension effects at model scale could corrupt the results if not properly accounted for.

3. Physical Interpretation

Consider a liquid jet of radius $r$ or a droplet of diameter $d$. Two competing forces act:

  • Inertial pressure: $Delta p_{inertia} sim
    ho v^2$ — dynamic pressure driving deformation
  • Laplace pressure: $Delta p_{Laplace} = 2sigma/r$ — excess pressure inside a curved interface resisting deformation

Their ratio for characteristic length $L = 2r = d$:

$$We = rac{
ho v^2 L}{sigma} sim rac{Delta p_{inertia}}{Delta p_{Laplace}}$$

We value Regime Interface behaviour Examples
We < 1 Surface-tension dominated Interface intact, droplet spherical Morning dew, soap bubble
We ~ 1 Transitional Droplet deforms but survives Light drizzle
1 < We < 12 Moderate inertia Deformation without breakup Moderate rain, dripping tap
We ≈ 12 Critical breakup Bag breakup onset for single droplet in airflow Windscreen raindrop
We >> 12 Inertia dominated Catastrophic breakup, atomisation Diesel injector, spray nozzle

4. Rayleigh–Plateau Instability — Jet Breakup

A cylindrical liquid jet of radius $r_0$ is always unstable to perturbations with wavelength $lambda > 2pi r_0$. Rayleigh (1879) showed that the fastest-growing perturbation has wavenumber $kr_0 pprox 0.697$, producing droplets of diameter:

$$d_{drop} pprox 1.89, d_{jet}$$

The growth rate of perturbations scales as $omega sim sqrt{sigma/(
ho r_0^3)}$. The Weber number controls whether the jet breaks in the dripping regime (low We, large droplets form near the nozzle) or the jetting regime (moderate We, jet extends several diameters before breaking) or the atomisation regime (high We, chaotic breakup very close to the nozzle).

Worked Example 1: Water Jet from a Garden Hose

A garden hose nozzle produces a jet of diameter $d_{jet} = 5$ mm at velocity $v = 3$ m/s. Water: $
ho = 1000$ kg/m³, $sigma = 0.073$ N/m.

Weber number:

$$We = rac{1000 imes 3^2 imes 0.005}{0.073} = rac{45}{0.073} = 616$$

Predicted drop diameter: $d_{drop} pprox 1.89 imes 5 ext{ mm} = 9.5 ext{ mm}$ (primary breakup estimate).

In reality, secondary aerodynamic breakup reduces this further since $We_{drop,air} =
ho_{air} v^2 d_{drop}/sigma = 1.2 imes 9 imes 0.0095/0.073 pprox 1.4$, just above critical for deformation. Final drop size ≈ 3–5 mm — consistent with garden-hose experience.

5. Droplet Breakup Mechanisms

When a droplet of liquid travels through a gas stream, the aerodynamic pressure distorts and ultimately fragments it. The breakup morphology depends on We:

We range Breakup mode Description
We < 12 None (stable) Droplet deforms but remains intact
12–18 Bag breakup Droplet inflates into a bag then bursts
18–45 Stripping / multimode Thin sheets stripped from droplet rim
45–350 Wave crest stripping Surface waves grow and shed ligaments
> 350 Catastrophic breakup Explosive fragmentation into fine mist

Worked Example 2: Rain Droplet Stability in a Storm

A raindrop of diameter $d = 4$ mm falls at terminal velocity $v_t pprox 9$ m/s. Will it break apart in air ($
ho_{air} = 1.2$ kg/m³, $sigma_{water} = 0.073$ N/m)?

$$We = rac{1.2 imes 9^2 imes 0.004}{0.073} = rac{0.389}{0.073} = 5.33$$

$We = 5.3 < 12$: the drop is stable against breakup but significantly deformed (oblate spheroid). This explains why natural raindrops are not perfectly spherical. Drops larger than ~5.5 mm would have We > 12 and break up, which is why observed raindrops rarely exceed 5–6 mm.

6. The Ohnesorge Number — Adding Viscosity

When viscosity is also important (e.g., in inkjet printing, polymer sprays, biological fluids), a third parameter is needed. The Ohnesorge number combines We and the Reynolds number Re:

$$Oh = rac{mu}{sqrt{
ho sigma L}} = rac{sqrt{We}}{Re}$$

$Oh$ compares viscous damping to the inertia–surface-tension restoring force. The Ohnesorge diagram (log$,Oh$ vs. log$,We$) maps the complete phase space of drop and jet behaviour into distinct regimes: dripping, jetting, and atomisation. This diagram is the primary design tool for inkjet nozzles, agricultural sprayers, and pharmaceutical inhalers.

The Dimensionless Trinity for Drop Dynamics

$$We = rac{
ho v^2 L}{sigma}, qquad Re = rac{
ho v L}{mu}, qquad Oh = rac{sqrt{We}}{Re} = rac{mu}{sqrt{
ho sigma L}}$$

  • Large We, small Oh: atomisation (diesel injector)
  • Small We, small Oh: dripping (slow faucet)
  • Intermediate We: stable jetting (Rayleigh regime)
  • Large Oh: viscous damping suppresses instability (honey)

Worked Example 3: Inkjet Printing Nozzle Design

An inkjet nozzle produces droplets of diameter $d = 25, mu ext{m}$ at velocity $v = 6$ m/s. Ink properties: $
ho = 1040$ kg/m³, $mu = 2 imes10^{-3}$ Pa·s, $sigma = 0.028$ N/m.

$$We = rac{1040 imes 36 imes 25 imes10^{-6}}{0.028} = rac{0.936}{0.028} = 33.4$$
$$Re = rac{1040 imes 6 imes 25 imes10^{-6}}{2 imes10^{-3}} = rac{0.156}{2 imes10^{-3}} = 78$$
$$Oh = rac{sqrt{33.4}}{78} = rac{5.78}{78} = 0.074$$

$Oh pprox 0.074$ is in the ideal inkjet printability window ($0.1 < 1/Oh < 10$, or equivalently $0.1 < Oh < 10$ with some authors using $Z = 1/Oh$). The drop forms cleanly without satellites at these parameters.

7. Bubble Formation

When gas is injected through an orifice into a liquid, the Weber number (based on gas velocity at the orifice) controls bubble size. For $We_{gas} < 2$, discrete spherical bubbles form at the orifice tip (bubbling regime). For $We_{gas} > 2$–$4$, a continuous gas jet penetrates the liquid and breaks into irregular bubbles (jetting regime). The transition is used to control bubble size in bioreactors, metallurgical furnaces, and aerators.

8. Drop Impact on Surfaces

When a droplet impacts a solid surface, the outcome depends on We and the surface wettability:

  • Spreading: We > 1; kinetic energy converts to surface energy as a thin lamella spreads outward
  • Bouncing: We << 1 on superhydrophobic surfaces; surface tension rebounds the droplet
  • Splashing: We > We_cr ≈ 80–500 (depending on surface roughness); unstable rim ejects secondary droplets

The maximum spreading diameter follows empirically:

$$ rac{d_{max}}{d_0} pprox 0.61(We + 12)^{1/3}$$

Worked Example 4: Raindrop Impact on a Leaf

Raindrop: $d_0 = 3$ mm, $v_{impact} = 7$ m/s, $
ho = 1000$ kg/m³, $sigma = 0.073$ N/m. Find maximum spread diameter.

$$We = rac{1000 imes 49 imes 0.003}{0.073} = rac{147}{0.073} = 2014$$
$$d_{max} = 0.61 imes d_0 imes (We + 12)^{1/3} = 0.61 imes 3 ext{ mm} imes (2026)^{1/3} = 1.83 imes 12.65 = 23.1 ext{ mm}$$

The 3 mm drop spreads to over 23 mm — nearly 8 times its initial diameter. This explains the characteristic splash rings visible in slow-motion photography of rain on flat surfaces, and why the Lotus leaf’s microstructure (reducing effective $sigma$) so dramatically limits spreading.

9. IYPT 2027 — Problem P7: Sinking Funnel

IYPT 2027 Problem P7: Sinking Funnel

A funnel is submerged mouth-downward in water, then slowly withdrawn. As water drains out of the funnel and air tries to enter, what happens at the air–water interface?

Weber number analysis: The critical parameter is the Weber number of water flowing out through the funnel throat of diameter $D$:

$$We_{throat} = rac{
ho_{water} v_{throat}^2 D}{sigma}$$

Regime 1 — We < 1: Surface tension stabilises the air–water interface. Air enters as discrete, well-separated bubbles at regular intervals. The interface is pinned to the funnel edge.

Regime 2 — We ~ 1: The interface oscillates and the bubble-entry pattern becomes irregular. This is the most photogenic regime for IYPT experiments.

Regime 3 — We > 1: Inertia dominates; a continuous air column enters and the water-air exchange becomes turbulent and chaotic.

The critical velocity for interface instability: $v_{cr} = sqrt{sigma / (
ho D)}$, giving $We_{cr} = 1$.
For a funnel throat $D = 20$ mm and water: $v_{cr} = sqrt{0.073/(1000 imes 0.02)} = sqrt{0.00365} = 0.060$ m/s = 6 cm/s.

10. Surface Tension Values and We at Standard Conditions

Fluid $sigma$ (N/m) at 20°C We at v=1 m/s, L=1 mm
Pure water 0.0728 13.7
Soapy water 0.025–0.040 25–40
Ethanol 0.0223 35.9
Mercury 0.485 27.6
Gasoline 0.021 34.3
Diesel fuel 0.027 31.5
Blood plasma 0.050 21.3

11. Diesel Fuel Atomisation

Modern diesel injectors operate at pressures of 2000–3000 bar, producing exit velocities of 300–600 m/s through orifices of 100–300 µm. The Weber number:

$$We = rac{
ho_{fuel} v^2 d_{nozzle}}{sigma_{fuel}} = rac{850 imes 300^2 imes 2 imes10^{-4}}{0.027} pprox 5.7 imes 10^5$$

This enormous Weber number (far exceeding the catastrophic breakup threshold of ~350) ensures complete atomisation into droplets of 5–20 µm within 1–2 mm of the nozzle exit. The resulting high surface area (relative to volume) enables complete combustion in the short time available during the engine cycle.

12. Weber Number in Pharmaceutical Aerosols

Inhaled drug delivery requires droplets of 1–5 µm to reach the alveoli. Pressurised metered-dose inhalers (pMDIs) and nebulisers exploit high We to atomise drug solutions. The challenge: We must be large enough to shatter the liquid into micron-scale droplets, but not so large that the droplets are too small (below 0.5 µm, droplets are exhaled without deposition). This narrow design window is navigated using the Ohnesorge diagram.

13. Related Dimensionless Numbers

Number Formula Physical meaning
Ohnesorge Oh $mu/sqrt{
ho sigma L}$
Viscous damping vs surface tension
Bond/Eötvös Bo $
ho g L^2/sigma$
Gravity vs surface tension (bubble rise)
Capillary Ca $mu v/sigma$ Viscous flow vs surface tension (porous media)
Morton Mo $gmu^4/(
ho sigma^3)$
Bubble shape in viscous liquids
Laplace La $
ho sigma L/mu^2 = We/Oh^2$
Surface tension vs viscosity²/inertia

14. Key Equations Summary

Weber Number Toolkit

  • Definition: $We =
    ho v^2 L / sigma$
  • Laplace pressure: $Delta p = 2sigma/r$ (single interface), $4sigma/r$ (soap bubble)
  • Critical droplet breakup in airflow: $We_{cr} pprox 12$
  • Rayleigh drop size: $d_{drop} pprox 1.89,d_{jet}$
  • Ohnesorge number: $Oh = sqrt{We}/Re$
  • Max spread diameter: $d_{max}/d_0 pprox 0.61(We+12)^{1/3}$
  • Sinking funnel critical speed: $v_{cr} = sqrt{sigma/(
    ho D)}$ (We = 1)
  • Bond number: $Bo = We/Fr^2 =
    ho g L^2/sigma$

15. Quick-Reference: Weber Number Across Applications

Application Typical We Regime / outcome
Morning dew on leaf < 0.1 Perfect sphere, no deformation
Raindrop (2 mm) 3–8 Stable, slightly oblate
Raindrop (5 mm) 30–60 Strongly deformed, near breakup
Dripping faucet 1–20 Rayleigh breakup, regular drops
Inkjet nozzle 10–100 Design operating window
Agricultural sprayer 50–300 Atomisation, 100–500 µm drops
Diesel injector $10^5$–$10^6$ Catastrophic atomisation, ~10 µm
Sinking funnel (IYPT P7) ~ 1 (transition) Discrete bubble vs. jetting
References:
1. Eggers, J., Villermaux, E. (2008). Physics of liquid jets. Reports on Progress in Physics, 71(3), 036601.
2. Rayleigh, Lord (1879). On the instability of jets. Proc. London Math. Soc. 10, 4–13.
3. Ashgriz, N. (ed.) (2011). Handbook of Atomization and Sprays. Springer.
4. Yarin, A.L. (2006). Drop impact dynamics. Annual Review of Fluid Mechanics 38, 159–192.
5. Hoath, S.D. (ed.) (2016). Fundamentals of Inkjet Printing. Wiley-VCH.
6. White, F.M. (2011). Fluid Mechanics, 7th ed. McGraw-Hill.
7. Cengel, Y.A., Cimbala, J.M. (2014). Fluid Mechanics: Fundamentals and Applications, 3rd ed. McGraw-Hill.

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