Air Prandtl Number Viscosity Heat Capacity Thermal Conductivity
Reference data and engineering information about air prandtl number viscosity heat capacity thermal conductivity for heat transfer applications.
airprandtlnumberviscosityCalculatorData Table
Overview
Engineering reference data for Air Prandtl Number Viscosity Heat Capacity Thermal Conductivity in heat transfer.
Key Formulas
Fourier's Law
Heat flux proportional to temperature gradient.
Convective Heat Transfer
Heat transfer between surface and fluid.
Stefan-Boltzmann Law
Radiative heat flux from a surface.
Thermal Resistance
Resistance to heat conduction.
Variables
| Symbol | Description | Unit |
|---|---|---|
| Heat flux | W/m² | |
| Thermal conductivity | W/(m·K) | |
| Convection coefficient | W/(m²·K) | |
| Temperature | K | |
| Emissivity | — | |
| Stefan-Boltzmann constant | 5.67×10⁻⁸ W/(m²·K⁴) |
10 rows
Temperature(°C) | Pr at 1 bara((-)) | Temperature(°F) | Pr at 1 bara((-)) |
|---|---|---|---|
| -100 | 0.734 | -150 | 0.733 |
| -50 | 0.72 | -50 | 0.719 |
| 0 | 0.711 | 0 | 0.714 |
| 25 | 0.707 | 60 | 0.709 |
| 50 | 0.705 | 75 | 0.708 |
| 100 | 0.701 | 100 | 0.706 |
| 150 | 0.699 | 200 | 0.701 |
| 200 | 0.698 | 300 | 0.699 |
| 250 | 0.699 | 400 | 0.698 |
| 300 | 0.702 | 500 | 0.7 |
Source: engineeringtoolbox.com
28 rows
Temperature(K) | Temperature(°C) | Temperature(°F) | Pr at 1 bara((-)) | Pr at 5 bara((-)) | Pr at 10 bara((-)) | Pr at 20 bara((-)) |
|---|---|---|---|---|---|---|
| 60 | -213.2 | -351.7 | 4.138 | 4.153 | 4.17 | 4.187 |
| 80 | -193.2 | -315.7 | 1.7 | 2.252 | 2.259 | 2.269 |
| 100 | -173.2 | -279.7 | 0.78 | 0.898 | 1.783 | 1.77 |
| 120 | -153.2 | -243.7 | 0.759 | 0.806 | 0.89 | 1.36 |
| 140 | -133.2 | -207.7 | 0.747 | 0.773 | 0.812 | 0.923 |
| 180 | -93.2 | -135.7 | 0.731 | 0.743 | 0.759 | 0.792 |
| 200 | -73.2 | -99.7 | 0.726 | 0.735 | 0.745 | 0.769 |
| 220 | -53.2 | -63.7 | 0.721 | 0.728 | 0.736 | 0.754 |
| 240 | -33.2 | -27.7 | 0.717 | 0.722 | 0.729 | 0.742 |
| 260 | -13.2 | 8.3 | 0.713 | 0.718 | 0.723 | 0.734 |
| 273 | 0 | 32 | 0.711 | 0.715 | 0.72 | 0.729 |
| 280 | 6.9 | 44.3 | 0.71 | 0.714 | 0.718 | 0.727 |
| 289 | 15.6 | 60 | 0.709 | 0.713 | 0.716 | 0.723 |
| 300 | 26.9 | 80.3 | 0.707 | 0.711 | 0.714 | 0.722 |
| 320 | 46.9 | 116.3 | 0.705 | 0.708 | 0.711 | 0.717 |
| 340 | 66.9 | 152.3 | 0.703 | 0.705 | 0.708 | 0.714 |
| 360 | 86.9 | 188.3 | 0.701 | 0.703 | 0.706 | 0.711 |
| 380 | 106.9 | 224.3 | 0.7 | 0.702 | 0.704 | 0.709 |
| 400 | 126.9 | 260.3 | 0.699 | 0.701 | 0.703 | 0.706 |
| 500 | 226.9 | 440.3 | 0.698 | 0.7 | 0.701 | 0.703 |
| 600 | 326.9 | 620.3 | 0.703 | 0.704 | 0.704 | 0.706 |
| 700 | 426.9 | 800.3 | 0.71 | 0.71 | 0.711 | 0.712 |
| 800 | 526.9 | 980.3 | 0.717 | 0.718 | 0.718 | 0.719 |
| 900 | 626.9 | 1160.3 | 0.724 | 0.725 | 0.725 | 0.725 |
| 1000 | 726.9 | 1340.3 | 0.73 | 0.73 | 0.73 | 0.731 |
| 1100 | 826.9 | 1520.3 | 0.734 | 0.735 | — | — |
| 1500 | 1226.9 | 2240.3 | 0.743 | 0.743 | — | — |
| 1900 | 1626.9 | 2960.3 | 0.742 | 0.742 | — | — |
Source: engineeringtoolbox.com
Prandtl Number Formula
The Prandtl number (Pr) is a dimensionless parameter defined as the ratio of momentum diffusivity (kinematic viscosity) to thermal diffusivity. It is fundamental in characterizing heat transfer in fluid flow.
Where:
- is the absolute or dynamic viscosity (kg/(m·s) or lbm/(ft·h))
- is the specific heat at constant pressure (J/(kg·K) or Btu/lbm·°F)
- is the thermal conductivity (W/(m·K) or Btu/(h·ft²·°F/ft))
Key Observations
- At atmospheric pressure (1 bara), air's Prandtl number is relatively constant (~0.71) over a wide temperature range (0°C to 300°C).
- Prandtl number increases significantly at very low temperatures and high pressures (e.g., Pr > 4 at 60 K and 1 bara).
- At standard conditions (0°C, 1 bara), Pr = 0.711 for air.