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February 9, 2011, 00:54 |
CFD Fluent Question
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#1 |
New Member
Gerardo Montano Uzcátegui
Join Date: Feb 2011
Posts: 2
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Hi everyone, im doing a Tesis with a NACA 0015 airfoil, and im studing the lift and drag coefficients, i need in my objectives comparate a grafic Cl vs angle of attack, and the same thing with the drag coefficient, i need a suport grafic to comparate my experimental results with the theoretical, who knows a page or something that contains this data? please! thanks
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February 9, 2011, 01:32 |
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#2 |
Senior Member
Join Date: Nov 2009
Posts: 411
Rep Power: 20 |
Abbott - Theory of Wing sections
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February 9, 2011, 15:10 |
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#3 |
New Member
Gerardo Montano Uzcátegui
Join Date: Feb 2011
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Thank´s, i really appreciate that reference, please if someone knows another page or book i will return the favor.
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February 14, 2011, 12:09 |
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#4 |
New Member
chris
Join Date: Feb 2011
Posts: 6
Rep Power: 15 |
That is the kind of thing you should easily be able to find in the above mentioned book.
Otherwise, google is your friend. |
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Tags |
airfoil, drag, fluent, lift, naca 0015 |
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