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{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: |
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This Page is Under Construction |
A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:
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3.4722e-7 kg/m*s |
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Using FLUENT, we will create a simulation of this experiment. Afterwards, we will compare values from the simulation and data collected from experiment. |
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Continue to {Step |
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1 - Pre-Analysis & Start-Up|ANSYS WB - Airfoil - Pre-Analysis & Start-Up} |