- #1
ruzfactor
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I have done a wind tunnel experiment on NACA 0015 airfoil for different angle of attack at a fixed velocity. Also calculated Cp, Cl, Cd and Cm for each angle of attack. Now I want to do an error analysis to find uncertainties in Cl,Cd and Cm. Please explain how I'm going to do that? I have searched google but couldn't find anything that made me clear about error analysis. The uncertainties should be in %of the total values.