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With our simulation data, we can now compare the Fluent with experimental data. The summary of result is shown in the table.
CL | Cd | |
FLUENT | 0.658 | -0.0112 |
Experiment - | 0.6 | 0.007 |
Theory | - | 0 |
| Info | ||
|---|---|---|
| ||
The experimental data is taken from Theory of Wing Sections By Ira Herbert Abbott, Albert Edward Von Doenhoff pg. 493 |
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