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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.


FLUENT

EXPERIMENT

Theory Value

4.5165 x 10^-5

Measured Value

~ 4.2 x 10^-5

Original Mesh

4.5167 x 10^-5

Lift Coeffient

 

0.663

Drag Coefficient

-0.0018097964

0.0090

Refined Mesh

4.5165 x 10^-5

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