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Problem Specification
A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:
Reynolds Number : 2.88e6
Angle of Attack : 6 degrees
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
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