Computational Flow Investigation on NACA 16-006 Airfoil at Varying Angle of Attack using Ansys Fluent. Acceleron Aerospace Journal, [S. l.], v. 5, n. 5, p. 1567–1584, 2025. DOI: 10.61359/11.2106-2561. Disponível em: https://acceleron.org.in/index.php/aaj/article/view/289. Acesso em: 7 mar. 2026.