Difference between revisions of "Contrib simpleScalarFoam"

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</math>
 
</math>
  
The mass transfer coefficient is determined at each wall by:
+
The mass transfer coefficient is determined at each wall by assuming that the value of ''T'' at the wall is zero:
  
<math>k_c=-\frac{D_T}{T_b-T_{wall}} \frac{\partial T}{\partial y}|_{y=0}</math>
+
<math>k_c=-\frac{D_T}{T_b} \frac{\partial T}{\partial y}|_{y=0}</math>
  
where <math>T_b</math> is the bulk value of ''T'', <math>T_{wall}</math> is the value of ''T'' at the wall and ''y'' is the direction normal to the wall.
+
where <math>T_b</math> is the bulk value of ''T'' and ''y'' is the direction normal to the wall.
  
 
The Sherwood number is then determined by:
 
The Sherwood number is then determined by:
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where ''d'' is the characteristic dimension.
 
where ''d'' is the characteristic dimension.
 +
 +
In order to use the solver, you should add <math>D_T</math>, <math>T_b</math> and ''d'' to the transportProperties dictionary.
  
 
== Download ==
 
== Download ==

Revision as of 12:36, 19 January 2009

Valid versions: OF version 15.png

1 Short description

A steady-state incompressible laminar flow solver with scalar transport and mass transfer coefficient and Sherwood number calculation.

2 Compilation

Do the following steps:

  • Download the solver package
  • tar xzf simpleScalarFoam.tar.gz
  • cd simpleScalarFoam
  • wmake

3 Physics

The solver is based on simpleFoam, with the transport of a scalar T having a mass diffusion coefficient D_T:

 
\nabla \cdot \left(\varphi T\right) - \nabla^2 \left( D_T \cdot T \right) = 0

The mass transfer coefficient is determined at each wall by assuming that the value of T at the wall is zero:

k_c=-\frac{D_T}{T_b} \frac{\partial T}{\partial y}|_{y=0}

where T_b is the bulk value of T and y is the direction normal to the wall.

The Sherwood number is then determined by:

Sh=\frac{k_c d}{D_T}

where d is the characteristic dimension.

In order to use the solver, you should add D_T, T_b and d to the transportProperties dictionary.

4 Download

The most up-to-date version of the sources can be downloaded below:


5 History

  • 2009-01-19: Initial upload