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← Airfoil Catalog
AS6092
Filename
as6092.dat
t/c
5.0%
Max Camber
5.4%
Download Selig Coordinates
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Reynolds Number
i
Include Mach Number
i
Yes
No
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Errors & Warnings
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GOE 494
t/c 5.0% · Max Camber 5.1%
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t/c 5.0% · Max Camber 5.8%
GOE 370
t/c 4.7% · Max Camber 5.7%
GOE 396
t/c 4.7% · Max Camber 5.8%
GOE 123
t/c 5.4% · Max Camber 5.7%
GOE 427
t/c 4.6% · Max Camber 5.7%
