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← Airfoil Catalog
GOE 741
Filename
goe741.dat
t/c
15.3%
Max Camber
4.8%
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Reynolds Number
i
Include Mach Number
i
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No
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t/c 15.4% · Max Camber 4.8%
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t/c 15.2% · Max Camber 4.5%
