Name
Begins with
OR
contains
AND
Maximum Lift (CL)between and  (at Re=100,000)
Maximum Lift-to-drag (L/D)between and
Thicknessbetween and
Camberbetween and
Maximum number to show:

Number of items found : 1524 (showing the first 50)

Name Thickness (%) Camber (%) Lift Coeff. Lift-to-Drag (L/D) Stall Angle (deg) TE Angle (deg) LE Radius (%)
YS-900 9.0 0.0 0.311 11.6 5.5 19.8 1.5
NACA M2 AIRFOIL 8.0 0.0 0.759 13.9 2.0 18.1 2.2
NACA-M1 AIRFOIL 6.2 0.0 0.644 12.4 1.5 17.4 1.9
LWK 80-150/K25 15.0 0.0 1.005 34.8 0.5 13.8 2.8
LWK 80-120/K25 12.1 0.0 0.861 36.9 6.5 14.3 2.3
WORTMANN FX L V-152 AIRFOIL 15.3 0.0 0.983 31.9 5.5 10.8 2.7
FX LIII-142 K 25 AIRFOIL 14.2 0.0 0.947 34.0 7.0 11.4 2.8
LWK 80-080 8.1 0.0 0.580 34.4 3.5 12.0 1.7
LWK 79-100 10.0 0.0 0.826 41.8 6.5 7.6 2.2
GOE 460 AIRFOIL 20.4 0.0 1.215 33.6 13.5 25.9 5.1
GOE 459 AIRFOIL 12.7 0.0 0.972 43.1 6.5 20.4 3.1
NASA/LANGLEY LS(1)-0013 AIRFOIL 12.8 0.0 0.977 27.9 7.0 20.9 2.8
FX 79-L-120 12.0 0.0 0.913 45.4 7.0 13.0 2.5
NACA M3 11.9 0.0 0.973 30.8 4.5 25.3 3.0
FX 79-L-100 10.0 0.0 0.795 51.1 5.5 11.7 2.1
NACA M2 8.1 0.0 0.760 14.0 2.0 20.1 2.2
GOE 445 AIRFOIL 6.4 0.0 0.552 40.2 4.0 10.3 1.6
GOE 444 AIRFOIL 5.6 0.0 0.515 31.6 3.5 10.3 1.5
GOE 443 AIRFOIL 5.0 0.0 0.512 30.1 3.0 7.4 1.5
EPPLER 297 AIRFOIL 11.3 0.0 0.625 50.8 4.5 7.2 2.0
FX 77-080 8.0 0.0 0.759 44.3 5.5 12.8 2.0
E230 (9.96%) 10.0 0.0 0.636 33.9 6.0 8.6 2.2
FX 76-120 12.0 0.0 0.963 41.9 8.0 16.7 2.8
FX 76-100 10.0 0.0 0.861 43.1 6.5 14.9 2.3
US1000ROOT 18.5 0.0 0.929 22.8 2.5 30.0 3.0
NACA 64A-010 10.0% 10.0 0.0 0.705 29.2 3.5 12.3 1.8
FX 71-L-150/30 AIRFOIL 15.0 0.0 0.962 25.3 0.5 9.8 2.9
FX 71-L-150/25 AIRFOIL 15.0 0.0 0.953 19.7 0.5 9.6 2.9
GOE 411 AIRFOIL 13.2 0.0 0.829 38.5 5.5 20.4 2.5
FX 71-L-150/20 AIRFOIL 15.0 0.0 0.947 19.1 0.5 9.1 2.9
GOE 410 AIRFOIL 15.9 0.0 1.039 30.9 9.0 10.3 4.5
WORTMANN FX 71-120 AIRFOIL 12.0 0.0 1.013 23.2 2.0 14.7 3.6
St. CYR 172 (Royer) 13.5 0.0 1.025 49.7 6.5 18.6 3.7
GOE 409 AIRFOIL 12.7 0.0 0.980 28.4 4.0 14.8 3.0
WORTMANN FX 71-089A AIRFOIL 8.9 0.0 0.931 11.2 1.0 11.0 2.8
E171 (Dicke 12.28%) 12.2 0.0 0.770 40.6 6.0 11.2 2.2
E169 (14.4%) 14.4 0.0 0.981 40.5 10.0 10.6 2.9
E168 (12.45%) 12.4 0.0 0.902 48.3 8.0 10.2 2.6
NACA 63(3)-018 18.0 0.0 1.067 28.9 10.5 6.7 3.3
HQ 0/9 AIRFOIL 8.1 0.0 0.552 34.0 4.0 5.8 1.8
HQ 0/7 AIRFOIL 7.0 0.0 0.475 29.5 3.0 5.0 1.6
HQ 0/10 AIRFOIL 10.0 0.0 0.685 36.8 5.5 7.2 2.0
NACA 16-021 20.9 0.0 1.142 32.8 0.5 56.2 3.8
Griffith 30% Suction Airfoil 30.5 0.0 1.588 29.1 1.5 13.0 4.7
NACA 16-018 17.9 0.0 1.068 33.5 0.5 49.3 3.2
NACA 16-015 14.9 0.0 0.956 29.8 5.0 41.9 2.7
NACA 16-012 12.0 0.0 0.812 25.3 3.5 34.1 2.3
NACA 16009 9.0 0.0 0.537 23.3 3.0 26.4 1.6
NACA 16-006 6.0 0.0 0.524 23.3 2.5 17.4 1.5
NACA 0024 23.9 0.0 1.284 25.3 3.0 40.6 7.1