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  • FLUENT - Flow over an Airfoil- Step 7

Versions Compared

Old Version 26

changes.mady.by.user user-8c4ec

Saved on

compared with

New Version 27

changes.mady.by.user user-8c4ec

Saved on

Key

  • This line was added.
  • This line was removed.
  • Formatting was changed.

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Original Mesh

Fine Mesh

%Dif

CL l

0.647

0.649

0.3%

Cd

0.00249

0.00137

45%

We see that the difference is fairly small and concluded that the original mesh is fine enough.

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