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← Airfoil Catalog
FX 66-S-161
Filename
fx66s161.dat
t/c
16.1%
Max Camber
3.9%
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Reynolds Number
i
Include Mach Number
i
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t/c 16.1% · Max Camber 3.9%
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t/c 16.0% · Max Camber 3.7%
AH 83-159
t/c 15.9% · Max Camber 3.8%
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t/c 16.0% · Max Camber 3.6%
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t/c 16.0% · Max Camber 4.2%
