'NACA 0012 Wing Section Case Study' simulation project by Ali_Arafat


#1

I created a new simulation project called 'NACA 0012 Wing Section Case Study':

Validation for NACA 0012


More of my public projects can be found here.


#2

NACA 0012 Wing Section - Airfoil Study

Mesh Domain

Results

Pressure Contours at AOA 10

Velocity Contours at AOA 10

Lift and Pressure Coefficient Plots