Khalid MH. CFD Analysis of NACA 0012 Aerofoil to Investigate the Effect of Increasing Angle of Attack on Coefficient of Lift and Coefficient of Drag. J. Stud. Sci. Eng. [Internet]. 2022 Mar. 31 [cited 2024 Nov. 21];2(1):74-86. Available from: https://engiscience.com/index.php/josse/article/view/josse2022216