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Knudsen Number Calculator — Mean Free Path & Flow Regime

The Knudsen number (Kn = λ/L) compares the molecular mean free path λ to the system's characteristic length L. It determines whether to model the gas as a continuous fluid (Navier-Stokes) or with kinetic/molecular theory — critical for MEMS, vacuum systems, microfluidics, and high-altitude aerodynamics.

K

Gas temperature in Kelvin (293 K = 20 °C)

Pa

Gas pressure in Pascals (101325 Pa = 1 atm)

m

Effective collision diameter (3.7×10⁻¹⁰ m for air / N₂)

m

Physical scale of interest: channel width, pore size, etc.
Knudsen number (Kn)
0.065640

Kn = mean free path λ / characteristic length L

Mean free path (λ)
6.5640e-8 m
λ in nanometres
65.64 nm
Flow regime
Slip flow — velocity-slip boundary conditions needed
Particle density illustration — higher density (more particles) means shorter mean free path and lower Kn
Step by step
  1. 1

    Collision cross-section area (π × d²)

    π × 0.00000000037² = 0
  2. 2

    Mean free path (λ = k_B × T ÷ (√2 × π × d² × P))

    k_B × 293 ÷ (√2 × π × 0.00000000037² × 101,325) = 0
    λ is the average distance a molecule travels between successive collisions.
  3. 3

    Knudsen number (Kn = λ ÷ L)

    0 ÷ 0.000001 = 0.065640
Results are estimates for general information only and are not professional advice — always verify important results independently before relying on them. Read the full disclaimer.
Quick answer

How does this calculator work?

Kn = λ / L where λ = k_B T / (√2 π d² P). At 20 °C / 1 atm, air has λ ≈ 66 nm. Kn < 0.001: continuum (Navier-Stokes). 0.001–0.1: slip flow. 0.1–10: transition (kinetic theory). Kn > 10: free-molecular. Defaults give Kn ≈ 0.066 — slip flow for a 1 µm channel in standard air.

Formula
Kn = λ / L • λ = k_B T / (√2 π d² P)
How this is calculated

The mean free path λ is the average distance a gas molecule travels between successive collisions. For an ideal gas it is λ = k_B T / (√2 π d² P), where k_B = 1.381 × 10⁻²³ J/K is the Boltzmann constant, T is temperature in kelvin, d is the effective collision diameter, and P is pressure. Raising T increases λ (faster molecules, less time between collisions in terms of path length); raising P decreases λ (more molecules per unit volume, more frequent collisions). At 20 °C and 1 atm, air has λ ≈ 66 nm.

The Knudsen number divides this by the characteristic length scale L of the problem — a channel width, pore diameter, MEMS gap, or aircraft chord at altitude. When Kn ≪ 0.001 the gas behaves as a continuum and classical Navier-Stokes equations apply with standard no-slip boundary conditions. In the slip-flow regime (0.001 < Kn < 0.1) the fluid equations still hold but velocity slip at walls must be included. In the transition regime (0.1 < Kn < 10) neither continuum nor free-molecular models are fully accurate; Boltzmann-equation solvers or DSMC (Direct Simulation Monte Carlo) are needed. Above Kn ≈ 10, gas behaves more like individual billiard balls than a fluid — free-molecular flow.

This calculator uses the hard-sphere ideal-gas model with a single-species effective diameter. Real gas mixtures require mixture-averaged collision integrals. The molecular diameter 3.7 × 10⁻¹⁰ m is the standard kinetic diameter for air (∼79% N₂, ∼21% O₂); for other gases, use tabulated kinetic diameters (e.g. He ≈ 2.6 × 10⁻¹⁰ m, CO₂ ≈ 4.0 × 10⁻¹⁰ m).

Frequently asked questions

The standard engineering boundaries are: Kn < 0.001 (continuum, Navier-Stokes valid), 0.001–0.1 (slip flow), 0.1–10 (transition / rarefied), Kn > 10 (free-molecular). These are rules of thumb — the transitions are gradual, not sharp, and exact thresholds vary by source.

MEMS features can be nanometres to micrometres in scale. At 1 atm, the mean free path for air is ≈ 66 nm, so a 1 µm channel gives Kn ≈ 0.066 — well into slip-flow territory. The classical no-slip boundary condition breaks down, causing measurable velocity slip, altered heat transfer, and higher-than-predicted flow rates.

Use the kinetic (hard-sphere collision) diameter, not the van der Waals radius. Common values: N₂ ≈ 3.7 × 10⁻¹⁰ m, O₂ ≈ 3.5 × 10⁻¹⁰ m, CO₂ ≈ 4.0 × 10⁻¹⁰ m, He ≈ 2.6 × 10⁻¹⁰ m, Ar ≈ 3.4 × 10⁻¹⁰ m, H₂ ≈ 2.9 × 10⁻¹⁰ m. For air use 3.7 × 10⁻¹⁰ m as an effective mean.

Also known as

knudsen number
mean free path calculator
gas flow regime calculator
rarefied flow knudsen
continuum slip transition free molecular
mems microfluidics flow regime
kinetic theory gas flow

APA

TG we-Calculate Editorial Team. (2026). Knudsen Number Calculator — Mean Free Path & Flow Regime [Online calculator]. TG we-Calculate. https://we-calculate.com/calculator/knudsen-number-calculator

Chicago

TG we-Calculate Editorial Team. "Knudsen Number Calculator — Mean Free Path & Flow Regime." TG we-Calculate. 2026. https://we-calculate.com/calculator/knudsen-number-calculator.

IEEE

TG we-Calculate Editorial Team, "Knudsen Number Calculator — Mean Free Path & Flow Regime," TG we-Calculate, 2026. [Online]. Available: https://we-calculate.com/calculator/knudsen-number-calculator

BibTeX

@misc{wecalculate_knudsen_number_calculator, title = {Knudsen Number Calculator — Mean Free Path & Flow Regime}, author = {{TG we-Calculate Editorial Team}}, howpublished = {\url{https://we-calculate.com/calculator/knudsen-number-calculator}}, year = {2026}, note = {TG we-Calculate} }

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