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April 24, 2010, 03:47 |
Reynolds Stress Turbulence Model
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#1 |
New Member
Cesar Laureti
Join Date: Apr 2010
Posts: 2
Rep Power: 0 |
Hi all
I trying to calculate the drag and lift of a low-reynolds high-lift airfoil using RSTM model, but i'm having problems to activate this model. What i should do??? Thanks all Cesar, from Brazil. PS:I tried k-e model but the airfoil have separations zone that the k-e model can't simulate correctly. The results with k-e were far of the experimental data. |
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April 26, 2010, 02:56 |
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#2 |
New Member
Join Date: May 2009
Location: Germany
Posts: 25
Rep Power: 17 |
Hi Cesar,
I havenīt worked with the reynold stress model yet but why donīt you set the RSTM = T in the Q1 file? like told in Polis: http://www.cham.co.uk/phoenics/d_pol...enc_r.htm#rstm Have you tried this and it didnīt work? Linh |
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December 2, 2010, 22:28 |
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#3 |
Member
Darren Leong
Join Date: Dec 2010
Posts: 64
Rep Power: 16 |
Hi Cesar,
I've only so far explored the rstm models using ANSYS CFX. The k-e model is highly sensitive to the grid density/y+ around the foil shape. I suggest that you do a grid independence study and apply a SST model if avalaible in pheonics. How far off were the results? ~15% is alright for initial validation of your model as the procedure's semi-blind unless you're really confident of your experiment data accuracy. -Dazza |
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Tags |
lift, rstm model, separation |
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