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← Airfoil Catalog
NACA 66(2)-215
Filename
naca662215.dat
t/c
15.0%
Max Camber
1.1%
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Reynolds Number
i
Include Mach Number
i
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NACA 63-215
t/c 15.0% · Max Camber 1.1%
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t/c 15.0% · Max Camber 1.0%
