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← Airfoil Catalog
CURTISS CR-1
Filename
cr1.dat
t/c
12.2%
Max Camber
4.7%
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Reynolds Number
i
Include Mach Number
i
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t/c 12.1% · Max Camber 4.6%
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t/c 12.0% · Max Camber 4.8%
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t/c 12.5% · Max Camber 4.8%
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t/c 12.4% · Max Camber 4.4%
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t/c 12.5% · Max Camber 4.9%
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t/c 12.6% · Max Camber 4.7%
