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PHYSICS

Prandtl Number Calculator — momentum versus thermal diffusivity

Work out the Prandtl number of a fluid from its specific heat, dynamic viscosity and thermal conductivity, and see the kinematic viscosity, thermal diffusivity and boundary-layer thickness ratio that follow from it.

Both routes give the same number. The first is what a property table gives you; the second is what a boundary-layer derivation gives you.
Density is not needed for the Prandtl number itself, only to split it into kinematic viscosity and thermal diffusivity. All four should come from the same table at the same temperature.
Used only to form the Péclet number, Pe = Re × Pr, which compares advected heat with conducted heat in the same flow.
Prandtl number Pr
 
 
0
Kinematic viscosity ν
0
Thermal diffusivity α
0
δ/δₜ ≈ Pr1/3
0
Péclet number Re·Pr
Tip: the Prandtl number is a property of the fluid alone. It does not know about your geometry, your flow speed or your surface. Those enter through the Reynolds and Nusselt numbers instead.
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The Prandtl number calculator above returns a single dimensionless quantity that describes a fluid, not a situation. Pr compares how fast momentum diffuses through a fluid with how fast heat diffuses through it. A high Prandtl number means momentum spreads more readily than heat; a low one means the opposite. Nothing about the pipe, the plate or the pump appears anywhere in it.

Arb Digital publishes free physics calculators that keep neighbouring quantities apart rather than blurring them. Three dimensionless groups get confused constantly in heat transfer, so it is worth stating the boundaries once and plainly. Pr is a fluid property. Nu is a heat-transfer result — the dimensionless convection coefficient you get out of a correlation for a specific flow, which the Nusselt number calculator handles. Bi compares internal conduction resistance with surface convection resistance in a solid body, which is what the Biot number calculator computes to decide whether a lumped-capacitance model is allowed.

What This Prandtl Number Calculator Does

Given specific heat, dynamic viscosity and thermal conductivity, it computes Pr = cpμ ÷ k. Add a density and it also reports the two diffusivities separately: kinematic viscosity ν = μ ÷ ρ, and thermal diffusivity α = k ÷ (ρcp). Their ratio is the same Prandtl number, computed a different way, which is a useful check that your property values are internally consistent.

The third output is the approximate ratio of the velocity boundary-layer thickness to the thermal boundary-layer thickness, which for laminar flow over a flat plate goes as Pr to the one-third. The fourth is the Péclet number, Re × Pr, if you supply a Reynolds number. Pe is the group that actually decides whether advection or conduction dominates the transport of heat in a flow, and it is where the fluid property and the flow condition finally combine.

How to Use It

  1. Pick your input route. Property tables usually give cp, μ and k, so that mode is the default. If you already have diffusivities, use the second mode and skip the conversion.
  2. Take all properties at the same temperature. Viscosity is strongly temperature-dependent and conductivity is not, so a mismatched pair can shift the Prandtl number by a large factor.
  3. Add a density if you want the diffusivities. The Prandtl number itself does not need it, because density cancels out of the ratio.
  4. Enter a Reynolds number if you have one. The Péclet number is the first genuinely situational quantity on the page.
  5. Use the boundary-layer ratio as a picture, not a design figure. The one-third power is a laminar flat-plate result and does not survive into turbulent flow or liquid metals unchanged.

The Formula: How the Prandtl Number Is Calculated

The definition is Pr = ν ÷ α, the ratio of momentum diffusivity to thermal diffusivity. Substituting ν = μ÷ρ and α = k÷(ρcp) makes the density cancel and gives the working form Pr = cpμ ÷ k. The random-walk treatment of viscosity and heat flow in Engineering LibreTexts defines the Prandtl number as exactly this dimensionless ratio ν÷κ, and gives the values that matter as anchors: close to 1 for air, where the three molecular diffusion constants are all about 1.5 × 10−5 m²/s, and about 7 for water.

The boundary-layer estimate follows from Blasius-type similarity solutions: for laminar flow over a flat plate the velocity layer and thermal layer thicknesses are related by δ÷δt ≈ Pr1/3 over the moderate-Pr range. NASA Glenn Research Center's boundary layer page describes the velocity layer that this comparison is made against, and gives the Reynolds number that governs its growth.

Work the defaults by hand. For water near 20 °C with cp = 4,182 J/kg·K, μ = 0.001002 Pa·s and k = 0.598 W/m·K, the product cpμ is 4.190364, and dividing by 0.598 gives Pr = 7.007. Check it the other way: ν = 0.001002 ÷ 998 = 1.0040 × 10−6 m²/s, and α = 0.598 ÷ (998 × 4,182) = 1.4328 × 10−7 m²/s. Their ratio is 7.007, the same number. The thickness ratio is 7.0071/3 = 1.914, and with Re = 5,000 the Péclet number is 35,036.

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What a Prandtl Number Actually Tells You

Read Pr as a statement about which boundary layer is thicker. When Pr is greater than one, momentum diffuses further than heat, so the velocity layer is thicker than the thermal layer and the temperature change is squeezed into a thin region right at the wall. That steep gradient is why high-Pr fluids like oils transfer heat well per unit of temperature difference at the surface, even though they are viscous and expensive to pump.

When Pr is much less than one, the thermal layer is far thicker than the velocity layer. Liquid metals sit here, with Prandtl numbers around 0.005 to 0.03, because their electrons conduct heat enormously well while their viscosity is unremarkable. Heat runs far ahead of the velocity profile, which is exactly why sodium and lead-bismuth are used as reactor coolants and why standard correlations fitted to water do not work for them.

Gases cluster near one, and that is not a coincidence. In a gas, the same molecular collisions that transport momentum also transport energy, so the two diffusivities come out comparable. Kinetic theory predicts a Prandtl number of order unity for simple gases, and measurement bears it out: air is close to 0.71 across a wide temperature range.

Pr, Nu and Bi: Three Numbers That Are Not Interchangeable

These three appear together constantly and mean entirely different things. The Prandtl number is a property of the fluid, fixed once you name the substance and the temperature. You look it up; you do not design it.

The Nusselt number is an outcome. It is the ratio of convective to conductive heat transfer at a surface, hL ÷ kfluid, and it is what a correlation such as Dittus-Boelter or Churchill-Bernstein returns when you feed it a Reynolds number and a Prandtl number for your specific geometry. Nu is where the flow, the shape and the fluid all meet, and the Nusselt number calculator is the page for it.

The Biot number is about a solid, not a fluid. It compares conduction resistance inside a body with convection resistance at its surface, hLc ÷ ksolid. Note the conductivity in the denominator: Nusselt uses the fluid's, Biot uses the solid's, and that single difference is what separates two formulas that otherwise look identical. The Biot number calculator uses it to judge whether a body can be treated as isothermal while it cools.

The usual chain of work runs in one direction. Get Pr from a property table. Get Re from the Reynolds number calculator for your flow. Feed both into a correlation to get Nu. Convert Nu into a convection coefficient h. Then, if you have a solid, use h to get Bi and decide how to model the transient.

How Temperature Moves the Number

Prandtl numbers for liquids are strongly temperature-dependent, almost entirely through viscosity. Water goes from around 13 at 0 °C to about 7 at 20 °C and under 2 at 100 °C, a sevenfold swing over the liquid range, because viscosity falls steeply while conductivity and specific heat barely move. Heavy oils change by orders of magnitude over an ordinary operating range.

Gases behave quite differently. Their viscosity and conductivity both rise with temperature at similar rates, so the ratio stays nearly flat: air is close to 0.71 from well below freezing to several hundred degrees. This is why a gas correlation can often be used with a single Prandtl number and a liquid correlation usually cannot.

Because of that, correlations for liquids frequently include a viscosity-ratio correction evaluated at the wall temperature as well as the bulk temperature. If you are entering property values here, decide which temperature you mean and use it consistently. The thermal conductivity calculator and the specific heat calculator cover the other two inputs, and the air viscosity calculator gives the temperature-dependent viscosity of air.

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Common Mistakes to Avoid

  • Mixing property temperatures — viscosity at one temperature and conductivity at another can shift the answer by a factor of several for a liquid.
  • Confusing dynamic with kinematic viscosity — the cpμ÷k form needs dynamic viscosity in Pa·s. Using ν there gives a number off by the density.
  • Treating Pr as a heat-transfer result — it is a fluid property. The heat transfer coefficient comes from Nu, and Nu needs a geometry and a flow.
  • Using water-fitted correlations for liquid metals — at Pr near 0.01 the thermal layer dwarfs the velocity layer, and correlations built for Pr near 1 to 10 do not extrapolate there.
  • Reading Pr1/3 as exact — it is a laminar flat-plate approximation for moderate Prandtl numbers, not a general result.

Related Free Tools From Arb Digital

Pair this with the Reynolds number calculator for the flow regime and the Nusselt number calculator for the convection coefficient that follows. The Biot number calculator handles the solid side of a transient problem. Property inputs come from the thermal conductivity calculator, the specific heat calculator, the air viscosity calculator and the density calculator. For the heat load itself, use the heat transfer calculator. Everything Arb Digital publishes is listed on the free online tools hub.

Frequently Asked Questions

What is the Prandtl number in simple terms?

It is the ratio of how fast momentum diffuses through a fluid to how fast heat diffuses through it. A value above one means the velocity boundary layer is thicker than the thermal one, and a value below one means the reverse.

Is the Prandtl number a fluid property or a flow property?

It is a fluid property. It depends only on the substance and its temperature, not on the geometry, the velocity or the surface. Flow information enters through the Reynolds number and the resulting Nusselt number instead.

What is the Prandtl number of water and air?

Water near 20 degrees Celsius is about 7, and air is close to 0.71 across a wide temperature range. Water's value falls steeply with temperature because its viscosity does, while air's stays nearly flat.

How is the Prandtl number different from the Nusselt number?

Prandtl is an input describing the fluid. Nusselt is an output describing a particular heat-transfer situation, equal to the convection coefficient times a length divided by the fluid conductivity. You typically use Reynolds and Prandtl in a correlation to obtain Nusselt.

How is the Prandtl number different from the Biot number?

Biot is about a solid body, comparing internal conduction resistance with surface convection resistance. It uses the solid's thermal conductivity, whereas Nusselt uses the fluid's, and Prandtl uses no geometry at all.

Why do liquid metals have such low Prandtl numbers?

Because free electrons carry heat extremely efficiently, giving a very high thermal conductivity, while the viscosity stays ordinary. Values around 0.005 to 0.03 are typical, which means heat diffuses far ahead of momentum.

What is the Péclet number and why is it shown here?

The Péclet number is the Reynolds number multiplied by the Prandtl number, and it compares heat carried by the flow with heat carried by conduction. It is the point at which the fluid property and the flow condition finally combine into one figure.

This tool is provided for educational and study use. It evaluates published definitions from the property values you supply and does not validate those values or account for variable-property, non-Newtonian or two-phase behaviour. The boundary-layer thickness ratio is a laminar flat-plate approximation. Treat the output as a physics result rather than a design-grade thermal figure.

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