Evaluating the Aerodynamic Performance of NACA2412 and NACA23012 Under Low-Angle Conditions
This article analyzes the aerodynamic characteristics of the NACA2412 and NACA23012 airfoils under low angles of attack. Computational fluid dynamics (CFD) numerical simulation is used to design geometric models and perform mesh generation, while the data were analyzed using a finite element method to calculate lift...