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 (%)
FX 77-W-270 27.0 4.3 0.283 2.1 -0.5 70.7 6.1
NACA 23021 21.0 2.4 0.443 6.6 7.5 44.5 4.9
NACA 2418 18.0 2.0 0.459 7.2 7.5 36.4 4.0
NACA 2421 21.0 2.0 0.501 7.3 7.5 42.4 4.7
NACA 2415 15.0 2.0 0.410 7.4 8.0 30.2 3.3
WORTMANN FX 77-W-343 AIRFOIL 34.2 4.7 1.374 9.4 -0.5 73.1 9.3
EPPLER 340 AIRFOIL 13.7 2.6 0.571 10.1 3.0 15.0 2.5
FX 79-W-470A 46.3 3.8 1.727 11.0 1.0 148.6 12.2
FX 79-W-660A 66.4 2.3 2.013 11.2 2.0 158.2 20.1
WORTMANN FX 71-089A AIRFOIL 8.9 0.0 0.931 11.2 1.0 11.0 2.8
AH 81-K-144 W-F KLAPPE 21.7 1.1 1.064 11.4 2.0 24.9 6.8
YS-900 9.0 0.0 0.311 11.6 5.5 19.8 1.5
NACA-M1 AIRFOIL 6.2 0.0 0.644 12.4 1.5 17.4 1.9
BOEING 707 .08 SPAN AIRFOIL 11.4 0.2 0.897 12.6 1.5 13.4 2.9
FX 77-W-270S 27.0 4.3 1.265 13.1 0.0 54.7 6.1
NACA 64-008A AIRFOIL 8.0 0.0 0.599 13.7 1.5 10.4 1.7
D.G.A. 1182 7.5 0.9 0.807 13.8 -0.5 15.3 1.8
EPPLER 864 STRUT AIRFOIL 38.8 0.0 1.384 13.8 3.0 61.4 10.9
NACA M2 AIRFOIL 8.0 0.0 0.759 13.9 2.0 18.1 2.2
NACA M2 8.1 0.0 0.760 14.0 2.0 20.1 2.2
EPPLER 863 STRUT AIRFOIL 35.7 0.0 1.326 14.2 2.5 55.0 9.8
ARA-D 20% AIRFOIL 20.0 3.7 1.539 14.5 1.5 56.5 5.7
EPPLER 862 STRUT AIRFOIL 32.3 0.0 1.318 14.8 2.0 48.0 8.7
BOEING-VERTOL VR-8 AIRFOIL WITH TAB 8.1 1.3 0.769 14.9 12.0 11.3 1.8
WORTMANN FX 77-W-258 AIRFOIL 26.1 4.3 1.652 15.8 -0.5 37.9 6.0
BOEING-VERTOL VR-9 AIRFOIL 6.0 0.3 0.540 15.8 9.5 6.3 1.6
NPL 9510 AIRFOIL 11.1 1.6 1.004 15.8 0.5 17.8 2.5
MH 78 14.47% 14.4 2.7 1.067 16.1 -0.8 6.3 3.7
E. Bambino 6.0 3.0 0.819 16.3 0.5 17.9 1.8
EPPLER 378 AIRFOIL 4.0 8.0 1.183 16.7 -0.5 2.8 1.8
BOEING 707 .19 SPAN AIRFOIL 12.2 0.7 1.114 16.9 1.5 13.8 2.7
AH 94-W-301 30.1 1.1 1.442 17.1 -0.5 53.4 7.3
AH 93-W-300 30.0 1.1 1.516 17.8 -0.5 48.4 10.8
HT05 4.8 0.0 0.590 18.0 2.5 16.8 1.7
NACA 66,2-(1.8)15.5 A=.6 P-51 ROOT AIRFOIL 15.5 1.3 1.049 18.4 -0.8 9.6 2.4
BOEING VERTOL V13006-.7 AIRFOIL 6.0 0.9 0.734 18.4 1.5 10.5 1.7
NASA SC(2)-0404 AIRFOIL 4.0 0.5 0.495 18.5 6.0 7.4 1.4
LA2573A 13.6 3.2 1.183 18.5 1.0 7.1 3.5
NASA/LANGLEY RC08-64C AIRFOIL 8.0 1.0 0.711 18.8 1.5 17.6 1.8
STRAND AIRFOIL 15.4 4.0 1.448 19.0 -0.5 0.3 3.3
NACA 63-206 6.0 1.1 0.539 19.0 -0.5 3.2 1.5
FX 71-L-150/20 AIRFOIL 15.0 0.0 0.947 19.1 0.5 9.1 2.9
HT08 5.0 0.0 0.581 19.3 3.0 12.7 1.7
NASA SC(2)-0403 AIRFOIL 3.0 0.4 0.408 19.4 5.0 6.3 1.3
WORTMANN FX 77-W-153 AIRFOIL 15.2 4.5 1.327 19.6 0.0 18.5 3.0
FX 71-L-150/25 AIRFOIL 15.0 0.0 0.953 19.7 0.5 9.6 2.9
NACA 23015 15.0 1.8 0.938 20.0 -0.5 32.4 3.3
BOEING AIRFOIL J 10.1 1.7 0.796 20.0 3.5 10.3 2.2
NASA SC(2)-0402 AIRFOIL 2.0 0.2 0.328 20.2 3.5 5.1 1.3
RAF 30 MOD AIRFOIL 7.6 0.0 0.696 20.2 2.0 8.9 2.0