{include: ANSYS WB - Airfoil - Panel}

{note}This Page is Under Construction{note}

A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:

Reynolds Number : 2.88e6
x velocity: 1 m/s
viscosity:  3.4722e-7 kg/m*s

Using FLUENT, we will create a simulation of this experiment. Afterwards, we will compare values from the simulation and data collected from experiment.

Continue to {Step 1 - Pre-Analysis & Start-Up|ANSYS WB - Airfoil - Pre-Analysis & Start-Up}