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  • Flow over an Airfoil - Verification & Validation

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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.


Unrefined Mesh

Refined Mesh FLUENT

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.

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