...
FLUENT | Data | |
---|---|---|
Lift Coeffient | 0.4998 6315 | 0.6630 |
Drag Coefficient | -0.0018 0122 | 0.0090 |
Below is a graph displaying the comparing Coefficient of Pressure along the airfoil for the experimental data and the CFD simulation.
...
...
FLUENT | Data | |
---|---|---|
Lift Coeffient | 0.4998 6315 | 0.6630 |
Drag Coefficient | -0.0018 0122 | 0.0090 |
Below is a graph displaying the comparing Coefficient of Pressure along the airfoil for the experimental data and the CFD simulation.
...