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← Airfoil Catalog
MH 115 11.06%
Filename
mh115.dat
t/c
11.1%
Max Camber
5.6%
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Reynolds Number
i
Include Mach Number
i
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N-10
t/c 11.2% · Max Camber 5.6%
GOE 363
t/c 11.1% · Max Camber 5.7%
GOE 358
t/c 10.9% · Max Camber 5.7%
N-11
t/c 10.9% · Max Camber 5.8%
GOE 323 (HANSA-BRANDENBURG V.1)
t/c 11.1% · Max Camber 5.2%
GOE 509
t/c 11.1% · Max Camber 5.2%
