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← Airfoil Catalog
NASA SC(2)-0503
Filename
sc20503.dat
t/c
3.0%
Max Camber
-0.7%
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Reynolds Number
i
Include Mach Number
i
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t/c 2.0% · Max Camber -0.5%
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t/c 4.0% · Max Camber 0.5%
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