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 Airfoil simulation, mismatch with theoretical data
Luigi Ferraro   |  14 days ago
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I simulated different airfoils with different AoA in order to compare simulation results with the data available on database

for some unknown reason I have got different results of Cl (lift coefficient). this is my procedure:

1 - get the airfoil shape from the database 

2 - import in solidworks and extrude (0.8m chord and 1m wing length, 0.8m2 area)

3 - simulate at

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