Latest revision as of 00:56, 24 February 2007

1 Test equation:

$C_f=\frac{\tau_w}{1/2\rho U_0^2}$ with $\tau_w=\mu\frac{\partial <u>}{\partial y} \Big|_{y=0}$

 
echo $PATH |grep OpenFOAM

My University Uvhc

Large Eddy simulation of an axisymmetric impinging jet on a circle plate.

Find a meshing strategie
Make the mesh for Large Eddy Simulation
First simulation with a steady impinging plate
Test the solution strategie with a rotating plate at various $\omega~(rad.s^{-1})$

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 My University [http://www.univ-valenciennes.fr Uvhc ]
+= Current Work: =
+Large Eddy simulation of an axisymmetric impinging jet on a circle plate.
+=== Problem setup ===
+[[Sketch of the computational domain:Exemple.jpg]]
+[[Boundary conditions:Exemple.jpg]]
+=== To do ===
+* Find a meshing strategie
+* Make the mesh for Large Eddy Simulation
+* First simulation with a steady impinging plate
+* Test the solution strategie with a rotating plate at various <math>\omega~(rad.s^{-1})</math>