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March 6, 2009, 10:31
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2D airfoil
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#1 |
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Guest
Posts: n/a
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Hi,
Does anybody has experience with computing the lift around an airfoil in 2D with Floworks? I am actually evaluating SW/Floworks for application in aircraft industry, but I didn't found any example As far as I was able to go, I found an error of more than 15% on the lift coefficient at low angles of attack.... Thank for help Etienne |
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