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Need help on boundary conditions on aerofoil simulations

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Old   May 3, 2009, 13:15
Default Need help on boundary conditions on aerofoil simulations
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LSC
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LSC
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Hi guys, need some advices on the boundary conditions on simulations of aerofoil. I have managed to mesh out the airfoils together with the computational domain. My domain consist of a semi circle encompassing the aerofoil and two rectangles downstream the airfoil. I am wondering is there any steps to define the boundary conditions as I am looking for the flow transition point. Do I have to select the turbulence model such as k-e or laminar? Please advice.
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