Flow analysis of air over a NACA airfoil at different angle of attack

Objective: This challenge is to analyse the flow of fluid over NACA0017 air foil at angle 0,2,4,6,8,10 degree and to compare the lift and drag force. steps followed: NACA0017 air foil (0017 indicates the thickness) curve is inserted from choose curve option. change entities option is used to change curve to a sketching…