Sulfur Dioxide Liquid Thermal Prorties

Reference data and engineering information about sulfur dioxide liquid thermal prorties for gases and compressed air applications.

Overview

Engineering reference data for Sulfur Dioxide Liquid Thermal Prorties in gases and compressed air.

$PV = nRT$

Pressure × Volume = moles × gas constant × temperature.

$P_1 V_1 = P_2 V_2$

At constant temperature.

$\frac{V_1}{T_1} = \frac{V_2}{T_2}$

At constant pressure.

Density: $1 \, \text{kg/m}^3 = 0.0624 \, \text{lb/ft}^3$
Specific Heat: $1 \, \text{kJ/kg K} = 0.2389 \, \text{kcal/(kg °C)} = 0.2389 \, \text{Btu/lb °F}$
Thermal Conductivity: $1 \, \text{W/(m K)} = 0.5779 \, \text{Btu/(ft h °F)}$
Dynamic Viscosity: $1 \, \text{Pa s} = 10 \, \text{Poise (P)} = 1000 \, \text{centipoise (cP)} = 0.1020 \, \text{kp s/m}^2 = 0.6721 \, \text{lb/(ft s)}$

The Prandtl Number (Pr) is a dimensionless number relating momentum and thermal diffusivity, defined as:

Pr = \frac{\mu c_p}{\lambda}

where $\mu$ is dynamic viscosity, $c_p$ is specific heat, and $\lambda$ is thermal conductivity.

The Reynolds Number (Re) for flow in a pipe is:

Re = \frac{\rho v D}{\mu}

where $\rho$ is density, $v$ is velocity, and $D$ is pipe diameter.

The Nusselt Number (Nu) for convective heat transfer often follows correlations of the form:

Nu = C \cdot Re^m \cdot Pr^n