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December 2, 2015, 07:25 |
Simulation of DU 97 W 300 2D Airfoil
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#1 |
New Member
daniele arlotti
Join Date: Jul 2015
Posts: 3
Rep Power: 11 |
hello everyone,
I'm doing simulation about DU 97 W 300 Airfoil 2D but i have some problem with the results ; I would like to know some parameters of the simulation : 1) the Chord of my airfoil is 0,6m : for the turbolent leght scale i have to use this value?(I'm using Spalart-Allmaras turbolent model) 2)I have to monitor the drag coefficient and the lift coefficient only on the airfoil wall top or also on the airfoil wall bottom? Thank you very much Daniele |
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