Muhammad, Ghassan Fadhil. “THE EFFECTS OF CYLINDER AT THE LEADING EDGE OF AIRFOIL NACA 0012 ON THE BOUNDARY LAYER SEPARATION”. Kufa Journal of Engineering 1, no. 2 (May 19, 2014): 72–88. Accessed August 6, 2026. https://journal.uokufa.edu.iq/index.php/kje/article/view/1297.