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← Airfoil Catalog
ULTIMATE
Filename
ultimate.dat
t/c
12.8%
Max Camber
-0.3%
Download Selig Coordinates
Run in Airfoil Model
Quick Analysis
Reynolds Number
i
Include Mach Number
i
Yes
No
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Errors & Warnings
Similar Airfoils
NASA/LANGLEY LS(1)-0013
t/c 12.9% · Max Camber 0.0%
GOE 409
t/c 12.7% · Max Camber 0.0%
GOE 459
t/c 12.7% · Max Camber 0.0%
EPPLER E836 HYDROFOIL
t/c 12.6% · Max Camber 0.0%
RAF 30
t/c 12.6% · Max Camber 0.0%
GOE 411
t/c 13.2% · Max Camber 0.0%
