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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

q=kTq = -k \nabla T

Heat flux proportional to temperature gradient.

Convective Heat Transfer

Q=hA(TsT)Q = hA(T_s - T_\infty)

Heat transfer between surface and fluid.

Stefan-Boltzmann Law

q=εσT4q = \varepsilon \sigma T^4

Radiative heat flux from a surface.

Thermal Resistance

Rth=LkAR_{th} = \frac{L}{kA}

Resistance to heat conduction.

Variables

SymbolDescriptionUnit
qqHeat fluxW/m²
kkThermal conductivityW/(m·K)
hhConvection coefficientW/(m²·K)
TTTemperatureK
ε\varepsilonEmissivity
σ\sigmaStefan-Boltzmann constant5.67×10⁻⁸ W/(m²·K⁴)
10 rows
Prandtl number for air at 1 bara pressure
Temperature(°C)
Pr at 1 bara((-))
Temperature(°F)
Pr at 1 bara((-))
-1000.734-1500.733
-500.72-500.719
00.71100.714
250.707600.709
500.705750.708
1000.7011000.706
1500.6992000.701
2000.6983000.699
2500.6994000.698
3000.7025000.7

Source: engineeringtoolbox.com

28 rows
Prandtl number for air at varying temperatures and pressures
Temperature(K)
Temperature(°C)
Temperature(°F)
Pr at 1 bara((-))
Pr at 5 bara((-))
Pr at 10 bara((-))
Pr at 20 bara((-))
60-213.2-351.74.1384.1534.174.187
80-193.2-315.71.72.2522.2592.269
100-173.2-279.70.780.8981.7831.77
120-153.2-243.70.7590.8060.891.36
140-133.2-207.70.7470.7730.8120.923
180-93.2-135.70.7310.7430.7590.792
200-73.2-99.70.7260.7350.7450.769
220-53.2-63.70.7210.7280.7360.754
240-33.2-27.70.7170.7220.7290.742
260-13.28.30.7130.7180.7230.734
2730320.7110.7150.720.729
2806.944.30.710.7140.7180.727
28915.6600.7090.7130.7160.723
30026.980.30.7070.7110.7140.722
32046.9116.30.7050.7080.7110.717
34066.9152.30.7030.7050.7080.714
36086.9188.30.7010.7030.7060.711
380106.9224.30.70.7020.7040.709
400126.9260.30.6990.7010.7030.706
500226.9440.30.6980.70.7010.703
600326.9620.30.7030.7040.7040.706
700426.9800.30.710.710.7110.712
800526.9980.30.7170.7180.7180.719
900626.91160.30.7240.7250.7250.725
1000726.91340.30.730.730.730.731
1100826.91520.30.7340.735
15001226.92240.30.7430.743
19001626.92960.30.7420.742

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.

Pr=μcpkPr = \frac{\mu c_p}{k}

Where:

  • μ\mu is the absolute or dynamic viscosity (kg/(m·s) or lbm/(ft·h))
  • cpc_p is the specific heat at constant pressure (J/(kg·K) or Btu/lbm·°F)
  • kk 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.

Interactive Charts

Prandtl number C

Prandtl number F