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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 | 0.658 647 | - 0.0112 00249 |
Experiment | 0.6 | 0.007 |
Theory | - | 0 |
| Info | |||||||
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The experimental data is taken from Theory of Wing Sections By Ira Herbert Abbott, Albert Edward Von Doenhoff pg. 493
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