Biot Number Calculator

The Biot number calculator helps you compute the Biot number that determines how quickly heat transfers from the surface of a body to its interior.

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Biot number0.0889the solid stays nearly uniform in temperature, so a lumped-capacitance model is valid
What it comparessurface convection ÷ internal conduction in the solida dimensionless group is always a ratio of two competing effects, and the number tells you which is winning
FormulaBi = hL ÷ k_solid
Characteristic length used20 mmthe choice of length is a convention, so figures are only comparable when it matches
Flow speed2 m/s
Kinematic viscosity ν1.004e-6 m²/sµ ÷ ρ — 1.0038 centistokes
Note on this group Below 0.1 is the licence to treat an object as having one temperature, which is why this number is checked before every transient cooling calculation.
Reynolds number (Re)39,848.3034inertial forces ÷ viscous forces
Mach number (Ma)0.0014flow speed ÷ speed of sound
Froude number (Fr)4.516inertia ÷ gravity
Prandtl number (Pr)0.0931momentum diffusivity ÷ thermal diffusivity
Knudsen number (Kn)3.4e-6molecular mean free path ÷ characteristic length
Weber number (We)1,096.9231inertia ÷ surface tension
Nusselt number (Nu)0.0889convective heat transfer ÷ conductive heat transfer
Péclet number (Pe)3,710.6421advective transport ÷ diffusive transport
Check: Re × Pr3710.64equals the Péclet number exactly, by definition

The formula

each group is a ratio of two competing effects

Why physics is done in ratios

A dimensionless group compares two competing effects, and its value says which one is winning. That is far more useful than either quantity alone, because it means a model aircraft in a wind tunnel and a real one in flight behave the same way provided their groups match. This is dynamic similarity, and it is the entire basis of scale testing.

The thresholds are where the physics changes character. Reynolds 2300 in a pipe is where smooth flow gives way to turbulence. Mach 0.3 is where air stops behaving as incompressible. Froude 1 is where a free surface can support a hydraulic jump, exactly as Mach 1 is where a shock becomes possible. Knudsen 0.01 is where treating a gas as a continuous fluid stops being valid at all.

Two cautions. The characteristic length is a convention, not a measurement — pipe diameter, aerofoil chord, plate length — so two Reynolds numbers are only comparable when both used the same one. And Nusselt and Biot look identical as formulas; the difference is that Nusselt uses the fluid's conductivity and Biot the solid's, which makes them answer completely different questions.