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November 18, 2010, 03:54
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Naca0012
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#1 |
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New Member
Join Date: Nov 2010
Posts: 7
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I WANT TO GET SOME INFORMATION ABOUT NACA0012 AT RE=50000(V=0.7239m/s),SUCH AS LIFT COEFFICIENT ,DRAG COEFFICIENT..
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November 18, 2010, 18:15
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#2 |
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Member
Michiel
Join Date: Jul 2009
Location: The Netherlands
Posts: 42
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November 18, 2010, 21:21
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#3 |
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Please click one of the Quick Reply icons in the posts above to activate Quick Reply.
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November 25, 2010, 20:01
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Thanks
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#4 |
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New Member
Join Date: Nov 2010
Posts: 7
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Hi,michiel
thanks for your help ,i am new about airfoil ,now ,i want to simulate naca0012 at re=50000,can you help me to set the turbulent kinetic energy and turbulent dissipation rate ？ thnks again manfeizhang |
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| drag coefficient, lift coefficient |
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