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Search: Posts Made By: louisgag
Forum: Main CFD Forum November 15, 2016, 11:24
Replies: 4
Views: 13,351
Posted By louisgag
For those looking for an answer to this simple...

For those looking for an answer to this simple but interesting question,
for all NACA symmetric airfoils, with the closed trailing edge, the center of mass is at roughly 0.3994*chord from the...
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