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Kumar R, Ghosh S. Aerodynamic Impacts of Convergent Slot Implementation on Hinged and Morphed NACA 0012 Airfoil Operating at a High Reynolds Number. Def. Sc. J. [Internet]. 2025 Jan. 10 [cited 2025 Aug. 18];75(1):3-9. Available from: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/19883