SpectraSim Documentation
Parameter · 04 Material

Sutherland coefficient As

material.compressible.sutherland.As Unit: kg/(m·s·√K) Step 04 · Material

The coefficient of Sutherland's viscosity law. Together with Sutherland temperature Ts it gives the gas viscosity at any temperature, for the incompressible solver (computed viscosity), the compressible solver (in every cell) and the heat-transfer correlations.

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Theory

Sutherland's law describes the rise of a gas's viscosity with temperature from a simple model of molecular attraction. In OpenFOAM's form, equation (1), AsA_s sets the level and TsT_s the curvature. The program uses the same constants for air and exhaust gas: the viscosity of exhaust gas is within a few per cent of that of air.

Equations

μ(T)=As T3/2T+Ts\mu(T) = \frac{A_s\,T^{3/2}}{T + T_s}
(1)
wheremeaningunit
μ\muDynamic viscosityPa s
AsA_sSutherland coefficient (this setting)kg/(m s K^0.5)
TsT_sSutherland temperatureK
TTTemperatureK

Default and rule

Default
1.458e-6 (air)
Rule

1.458e-6 kg/(m s K^0.5), which with TsT_s = 110.4 K gives air's viscosity: 1.81e-5 Pa s at 20 °C.

Source

Sutherland's law (Sutherland, 1893); the air constants are those of the standard atmosphere (U.S. Standard Atmosphere, 1976). The compressible solver receives them as transport sutherland in constant/thermophysicalProperties.

Valid range > 0

Values

Positive. Change it only for a gas other than air or exhaust gas.

References 2

  1. Sutherland, W. (1893). The viscosity of gases and molecular force. The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, 36(223), 507-531. DOI 10.1080/14786449308620508
  2. NOAA, NASA and USAF (1976). U.S. Standard Atmosphere, 1976. NOAA-S/T-76-1562, NASA-TM-X-74335. Web page