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← Airfoil Catalog
CR001 (smoothed)
Filename
cr001sm.dat
t/c
7.3%
Max Camber
4.1%
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Reynolds Number
i
Include Mach Number
i
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GOE 122 (MVA H.2)
t/c 7.3% · Max Camber 4.1%
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t/c 7.3% · Max Camber 4.0%
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t/c 7.3% · Max Camber 4.0%
GOE 278 (DAIMLER IX)
t/c 7.4% · Max Camber 4.3%
I.S.A. 571
t/c 7.4% · Max Camber 4.3%
A18 (smoothed)
t/c 7.3% · Max Camber 3.8%