Knudsen Number Calculator

Calculate the Knudsen number to determine gas flow regime — continuum, slip, transition, or free molecular — from mean free path and characteristic length.

Knudsen Number
6.800e-8
Kn = λ / L
Flow Regime
Continuum Flow
Navier-Stokes equations valid
Mean Free Path
68.0 nm
= 0.0680 µm
Characteristic Length
1 m
Relevant length scale (pipe dia, plate length, gap, etc.)
Equivalent Reynolds (1/Kn)
14,705,882.35
Rough continuum equivalent; not a true Reynolds number
log₁₀(Kn)
-7.167
Useful for regime classification
Regime Indicator
Continuum
Slip
Transition
Free Mol.
Kn RangeRegimeMethodExample
Kn < 0.01ContinuumNavier-StokesEveryday aerodynamics
0.01 < Kn < 0.1Slip FlowN-S + slip BCsMicrofluidics, low-P gaps
0.1 < Kn < 10TransitionDSMC, BoltzmannHigh-altitude flight
Kn > 10Free MolecularMolecular dynamicsOuter space, vacuum process
Planning notes, formulas, and examples

About the Knudsen Number Calculator

The Knudsen number (Kn) is a dimensionless number that determines which physical model best describes gas flow in a given situation. Defined as the ratio of the molecular mean free path to the characteristic length of the system, it tells you whether molecules interact primarily with each other (continuum flow) or with the walls of the system (free molecular flow).

At everyday scales and pressures, Kn is tiny and the familiar Navier-Stokes equations work perfectly. But in microfluidics, vacuum systems, high-altitude flight, and space environments, Kn can become large enough to require specialized methods like DSMC (Direct Simulation Monte Carlo) or molecular dynamics.

This Knudsen Number Calculator computes Kn from the mean free path and characteristic length, identifies the flow regime, and provides a visual regime indicator. You can either enter the mean free path directly or compute it from temperature, pressure, and molecular diameter. Preset buttons cover applications from Standard atmosphere to vacuum chambers and re-entry vehicles. A regime comparison table summarizes the modeling approaches for each range.

When This Page Helps

Use This calculator to decide whether a gas-flow problem can be treated as continuum flow or whether you need slip corrections, transition models, or rarefied-gas methods. It gives a quick regime check before you choose a CFD, slip-flow, or molecular model. That makes it easier to match the flow regime to the solver before you start the analysis.

How to Use the Inputs

  1. Enter the characteristic length of your system (pipe diameter, gap, device size, etc.) in meters.
  2. Select whether to enter the mean free path directly or compute it from gas properties.
  3. If computing: enter temperature (K), pressure (Pa), and molecular diameter (m).
  4. If direct: enter the mean free path in nanometers.
  5. Review the Knudsen number, flow regime, and regime indicator.
  6. Consult the regime table for the appropriate modeling method.
Formula used
Kn = λ / L Mean Free Path: λ = kT / (√2 × π × d² × P) k = 1.381 × 10⁻²³ J/K (Boltzmann constant) d = molecular diameter Regimes: Kn < 0.01 continuum; 0.01–0.1 slip; 0.1–10 transition; > 10 free molecular

Example Calculation

Result: Kn = 6.8 × 10⁻⁸, Continuum Flow

Air at standard conditions has a mean free path of ~68 nm. In a 1 m pipe, Kn is vanishingly small — solidly in the continuum regime.

Tips & Best Practices

  • Knudsen number becomes important either when the system gets very small or when the gas gets very thin.
  • Microchannels can enter slip or transition flow even at modest temperatures if pressure is low enough.
  • At high altitude, continuum assumptions break down gradually rather than all at once, so regime boundaries are guidance rather than magic cutoffs.
  • If Kn is comfortably below 0.01, standard continuum CFD with no-slip walls is usually the starting point.

Why Knudsen Number Matters

The Knudsen number compares mean free path with system size. When the mean free path is tiny relative to the geometry, collisions between molecules dominate and continuum fluid mechanics works well. As Kn grows, wall interactions and non-equilibrium effects become too important to ignore.

Regime Interpretation

Continuum flow generally supports Navier-Stokes with no-slip walls. Slip flow still uses continuum equations, but the wall boundary condition changes. Transition flow is harder because neither continuum nor free-molecular descriptions are fully satisfactory on their own. Free molecular flow is the regime where molecules interact with boundaries far more often than with each other.

Modeling Caution

The exact regime boundaries are practical rules of thumb, not universal physical discontinuities. Surface accommodation, geometry, gas species, and the output you care about can all shift which model is acceptable.

Sources & Methodology

Last updated:

Frequently Asked Questions

  • The average distance a molecule travels between collisions with other molecules. It depends on temperature, pressure, and molecular size, so it can change a lot with operating conditions.