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Forum: Questions
4th Jan 2018, 04:07
Replies: 8
Views: 2,454
Posted By megan

I'm obviously missing some thing here. I thought...

I'm obviously missing some thing here. I thought Cl(max) was a function of the particular airfoil eg NACA 2410 a little over 2.4 at a Reynolds 6X10^6. I thought angle of attack was the sole key,...
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