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To validate our data, we will take a compare the data from actual experiment. Much thanks to David Caughey for providing us with the experimental data.
|
FLUENT |
Data |
|---|---|---|
Lift Coeffient |
0.4998 |
0.6630 |
Drag Coefficient |
-0.0018 |
0.0090 |
Below is a graph displaying the comparing Coefficient of Pressure along the airfoil for the experimental data and the CFD simulation.
