Click here to see an enlarged image
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.
Click here to see an enlarged image
Go to all FLUENT Learning Modules