Numerical Analysis of Flow Over NACA0012 at Fixed Mach Number using Computational Fluid Dynamics

Abstract

In this present work, we carry out a numerical analysis of lift and drag performances of NACA0012 airfoil at various angles of attack, by using computational fluid dynamic software. We can also utilize wind tunnel testing setup, to determine lift and drag force. In this investigation process, the design model has to be placed in the test section.