Air Viscosity by Sutherland's Law

Also known as Sutherland's law · Sutherland's formula · viscosity of air from temperature · dynamic viscosity of air · mu of air · air viscosity at altitude · air viscosity for Reynolds number · Sutherland constant 110.4 · viscosity of air in the standard atmosphere · how thick is air · viscosity of air at 15 degrees · gas viscosity temperature law

μ=β T3/2T+S\mu = \frac{\beta\,T^{3/2}}{T + S}

or type the values yourself

sig figs

Worked example: U.S. Standard Atmosphere 1976 Table III, Z = 0: 288.15 K → 1.7894e-5 N s/m2. Press Try an example to run it live, then adjust anything.

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Where Air Viscosity by Sutherland's Law fits

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See also

Reynolds Number: Takes this viscosity, with the air density, a speed and a length, to the Reynolds number of the wind past an object.Standard Atmosphere Density (Troposphere): The air density that goes with the same temperature and pressure, to make the kinematic viscosity or a Reynolds number.Moist Air Density at Altitude (and the 1.08 Correction): The density of the actual, humid air at an airport, which the Reynolds number wants beside this viscosity.
Learning zone

Air Viscosity by Sutherland's Law explained

proportionalμT

Dynamic viscosity measures how strongly a fluid resists being sheared, and for air it is the one property a Reynolds number for the wind past an object needs that a weather report does not give. This page finds it from the absolute temperature alone. Air gets more viscous as it warms, the opposite of a liquid, because a gas carries momentum by molecules colliding. Pressure does not appear in the equation, and the standard's own table uses it from sea level to 86 km.

The equation is μ=βT3/2/(T+S)\mu = \beta T^{3/2}/(T+S), with β=1.458×10−6\beta = 1.458\times10^{-6} kg/(m s K^(1/2)) and Sutherland's constant S=110.4S = 110.4 K. Because SS is a temperature that is added to TT, the temperature must be absolute, so the page works in kelvins and the unit pickers convert from degrees Celsius or Fahrenheit. The two constants are the values the standard prints. This is a working formula, not an exact law: the standard itself warns that it fails at very low and very high temperatures and at great heights, so treat answers far outside the weather range as extrapolation.

The source is the U.S. Standard Atmosphere, 1976 (NOAA, NASA and the U.S. Air Force), which prints this as equation 51 and builds its table of viscosity by height from it. The page agrees with that table. At 288.15 K (15 degrees Celsius) it gives 1.78938×10−51.78938\times10^{-5} Pa s, where the table prints 1.7894×10−51.7894\times10^{-5}. At 216.65 K, the cold air at 11 to 20 km, it gives 1.42161×10−51.42161\times10^{-5} against 1.4216×10−51.4216\times10^{-5}. Two more rows, at 223.254 K and 236.215 K (temperatures from the standard's lapse of 6.5 K per km in the lowest layer), give 1.45767×10−51.45767\times10^{-5} and 1.52711×10−51.52711\times10^{-5} against the printed 1.4577×10−51.4577\times10^{-5} and 1.5271×10−51.5271\times10^{-5}. The table prints five significant figures, so the agreement is to that precision.

Once you have the viscosity, divide by the air density for the kinematic viscosity, or put it in a Reynolds number with a speed and a length. As a hand check by a different route, at 300 K the equation gives 1.846×10−51.846\times10^{-5} Pa s, a little above the 15 degree value because the air is warmer.

Air Viscosity by Sutherland's Law formula

μ=β T3/2T+S\mu = \frac{\beta\,T^{3/2}}{T + S}
Where
  • μ\mu= Dynamic viscosity of the air (Pa·s)
  • TT= Absolute temperature of the air (°C)
Where this comes from
  • National Oceanic and Atmospheric Administration, National Aeronautics and Space Administration and United States Air Force, U.S. Standard Atmosphere, 1976 (NOAA-S/T 76-1562, NASA TM X-74335), Washington, D.C., October 1976; public domain. Section 1.3.11 Dynamic Viscosity, equation 51, mu = beta T^(3/2)/(T + S) with beta = 1.458 x 10^-6 kg/(s m K^(1/2)) and S = 110.4 K (printed page 19); Table III, Geometric Altitude and Geopotential Altitude, Metric Units, the dynamic viscosity column in N s/m2 (printed pages 101 to 108): 1.7894 x 10^-5 at Z = 0 m; 1.5612, 1.5271 and 1.4577 x 10^-5 at Z = 7,000, 8,000 and 10,000 m; 1.4216 x 10^-5 at H = 19,000 m. Read it
Revised 31 October 2026
Cite this page

formula.expert. (2026, October 31). Air Viscosity by Sutherland's Law Formula & Calculator. https://formula.expert/solvers/air-viscosity-sutherland