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← Airfoil Catalog
NACA 64(1)-112
Filename
naca641112.dat
t/c
12.0%
Max Camber
0.6%
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Reynolds Number
i
Include Mach Number
i
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R140 (original)
t/c 12.0% · Max Camber 0.5%
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t/c 12.1% · Max Camber 0.7%
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t/c 12.1% · Max Camber 0.7%
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t/c 12.0% · Max Camber 0.4%
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t/c 12.0% · Max Camber 0.9%
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t/c 12.2% · Max Camber 0.9%