We developed this project during my undergraduate studies at EAFIT University. We analyzed the evolution of an initial blunt object (rectangle) into a NACA airfoil. The transition was conducted by examining fluid mechanics indicators such as lift, drag, streamline curvature, and pressure difference.

• StackMatlab, Ansys
• Publication PDFUIS Ingenierías
• CitationCristian C. Rendon, Jose L. Hernandez, Oscar Ruiz – Salguero, Carlos A. Alvarez, Mauricio Toro. Vol. 18 , n. 2, pp. 139-146, 2019 Revista UIS Ingenierías, ISSN printed: 1657-4583, ISSN (online): 2145-8456, url: https://revistas.uis.edu.co/index.php/revistauisingenierias/article/view/9031, , doi: 10.18273/revuin.v18n2-2019013. Published online: 2019-02-14 .