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← Airfoil Catalog
NACA 66(3)-218
Filename
naca663218.dat
t/c
18.0%
Max Camber
1.1%
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Reynolds Number
i
Include Mach Number
i
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NACA 63(3)-218
t/c 18.0% · Max Camber 1.1%
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t/c 18.0% · Max Camber 1.1%
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t/c 18.0% · Max Camber 1.2%
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t/c 18.0% · Max Camber 1.8%
