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← Airfoil Catalog
NACA M12
Filename
m12.dat
t/c
11.9%
Max Camber
2.0%
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Reynolds Number
i
Include Mach Number
i
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GOE 676 (= M 12)
t/c 11.9% · Max Camber 2.0%
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t/c 12.0% · Max Camber 2.0%