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CL | Cd | ||||
---|---|---|---|---|---|
FLUENT | 0.647 | 0.00249 | |||
Experiment | 0.6 | 0.007 | |||
% Dif | 7.8% | 64% | Theory | - | 0 |
Though further validation steps are still needed before we can come up with a model that will accurately represent the physical flow, this simple tutorial demonstrates the use of reasonable assumption and approximation in obtaining understanding of physical flow properties around an airfoil.
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