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← Airfoil Catalog
NACA 65(4)-421 a=0.5
Filename
naca654421a05.dat
t/c
21.0%
Max Camber
3.0%
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i
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AH 93-W-215
t/c 21.2% · Max Camber 3.1%
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NACA 63(4)-421
t/c 21.0% · Max Camber 2.2%
NACA 65(4)-421
t/c 21.0% · Max Camber 2.2%
NACA 64(4)-421
t/c 20.9% · Max Camber 2.2%
NASA/LANGLEY LS(1)-0421MOD
t/c 21.0% · Max Camber 2.1%
