KUMAR, R.; GHOSH, S. Aerodynamic Impacts of Convergent Slot Implementation on Hinged and Morphed NACA 0012 Airfoil Operating at a High Reynolds Number. Defence Science Journal, [S. l.], v. 75, n. 1, p. 3–9, 2025. DOI: 10.14429/dsj.19883. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/19883. Acesso em: 18 aug. 2025.