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Unrefined Mesh | Refined Mesh | Data | |
|---|---|---|---|
Lift Coeffient | 0.6315 | 0.6670 | 0.6630 |
Drag Coefficient | - 0.0122 | 0.0063 | 0.0090 |
Below is a graph displaying the comparing Coefficient of Pressure along the airfoil for the experimental data and the CFD simulation.
Click here to see an enlarged image
As we can see from the table and the graph, the CFD has provided us very valuable data. Although there is an error associated with the