SimScale simulation projects by billymc7601 | Page 1

billymc7601's profile

In this project we examined the Effect of Boundary Layers on the  NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A  10 with the airfoil. - Copy

This project has expanded a bit to include the following:
-Result validation of NACA0012
-icing of NACA0012
-Turbulence model comparison (LES and RANS) for NACA0012 - Copy

Public Profile

billymc7601's profile