Flow over NACA0008 for various Angles of attack

Objective: Google drive link to all the contours and plot: https://drive.google.com/open?id=1fBI5Zcassvv2ut9o2Qsy7ktrIq3LQx10 The link contains all the plots for various angles of attack and the pressure and velocity distribution for all cases. The airfoil used was NACA0008. A chord length of 0.5m was used for the wing with…