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  • FLUENT - Flow over an Airfoil- Step 7

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Following table shows comparison of modeling result with experimental data.


CL l

Cd

FLUENT

0.647

0.00249

Experiment

0.6

0.007

% Dif

7.8%

64%


CL l

Cd

FLUENT Fine Mesh

0.649

0.00137

Experiment

0.6

0.007

Theory

-

0

...