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 (%)
Marsden 27.8 9.6 2.809 59.3 -5.5 8.6 8.8
KFm3-TGK 11.3 5.7 1.598 316.5 -5.0 58.0 2.1
KFm2-TGK 8.8 4.4 1.502 281.2 -5.0 58.0 2.0
GOE 525 AIRFOIL 16.4 9.7 2.712 83.1 -4.0 8.6 4.8
GOE 523 AIRFOIL 16.4 9.7 2.712 83.1 -4.0 8.6 4.8
EPPLER 479 AIRFOIL 16.6 0.0 1.097 35.2 -1.1 12.2 3.8
E487 15.7 0.0 1.031 39.4 -1.0 12.4 3.4
EPPLER 1213 AIRFOIL 17.3 2.1 1.268 28.7 -0.9 12.0 4.6
MH 93 15.98% 16.0 1.7 1.113 31.6 -0.9 8.2 3.2
EPPLER 1214 AIRFOIL 19.8 2.1 1.333 22.7 -0.9 15.3 4.9
MH 92 15.49% 15.5 1.7 1.115 33.0 -0.8 7.8 3.1
EPPLER E1212MOD AIRFOIL 17.7 2.6 1.470 31.6 -0.8 12.9 4.6
MH 91 14.98% 15.0 1.7 1.114 35.3 -0.8 7.6 3.0
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
MH 78 14.47% 14.4 2.7 1.067 16.1 -0.8 6.3 3.7
EPPLER E1212 AIRFOIL 17.7 3.2 1.470 37.0 -0.7 11.8 4.5
MH 102 16.99% 17.0 3.0 1.510 39.7 -0.7 13.2 3.5
ARA-D 13% AIRFOIL 13.0 3.6 1.421 28.4 -0.7 46.5 3.8
MUE 139 13.9 4.7 1.526 45.6 -0.6 16.2 4.2
USA 45 AIRFOIL 14.4 4.1 1.477 47.9 -0.6 16.4 3.6
NASA/LANGLEY LS(1)-0421MOD AIRFOIL 20.9 2.1 1.759 33.4 -0.6 25.4 5.4
EPPLER 1230 AIRFOIL 17.4 3.6 1.619 49.5 -0.6 24.1 3.4
GOE 769 AIRFOIL 13.8 4.8 1.506 41.5 -0.5 11.3 5.0
SD7062 (14%) 14.0 4.0 1.589 52.5 -0.5 7.5 3.5
EPPLER 1211 AIRFOIL 18.0 4.4 1.671 45.5 -0.5 11.9 5.2
NACA M23 AIRFOIL 8.1 6.3 1.197 27.7 -0.5 22.1 2.1
GOE 500 AIRFOIL 9.9 6.0 1.565 67.0 -0.5 8.2 2.7
YS-930 9.1 3.0 0.839 45.0 -0.5 14.2 1.8
NACA M22 AIRFOIL 6.2 6.3 1.068 31.4 -0.5 19.3 1.8
GOE 499 AIRFOIL 6.8 5.8 1.307 71.3 -0.5 6.0 2.0
YS-915 9.1 1.8 0.612 34.0 -0.5 15.0 1.6
NACA M21 AIRFOIL 11.9 6.0 1.446 30.3 -0.5 26.8 3.1
NACA 66,2-(1.8)12 A=.6 P-51 TIP AIRFOIL 12.0 1.3 0.897 30.5 -0.5 7.9 2.0
WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL 11.0 2.3 1.209 45.5 -0.5 2.9 3.0
EPPLER 417 AIRFOIL 14.2 3.2 1.275 67.7 -0.5 11.0 2.2
WB-140/35/FB 14% 13.9 3.7 1.409 88.6 -0.5 27.8 3.0
P-51D TIP (BL215) AIRFOIL 11.4 1.3 0.830 39.9 -0.5 6.9 1.9
EPPLER 407 AIRFOIL 14.4 3.5 1.449 70.2 -0.5 8.0 2.2
GOE 494 AIRFOIL 4.9 5.1 1.144 76.7 -0.5 5.5 1.7
EPPLER 403 AIRFOIL 14.9 3.3 1.421 64.4 -0.5 7.3 2.3
GOE 482 AIRFOIL 16.4 8.8 2.297 60.0 -0.5 8.9 4.7
FX S 03-182 AIRFOIL 18.2 2.8 1.337 42.1 -0.5 9.2 2.6
FX S 02-196 AIRFOIL 19.6 3.7 1.589 58.0 -0.5 6.6 3.1
EPPLER 379 AIRFOIL 2.2 8.0 0.545 73.3 -0.5 2.8 1.7
EPPLER 378 AIRFOIL 4.0 8.0 1.183 16.7 -0.5 2.8 1.8
NN7 MK20 16.8 3.0 1.415 49.0 -0.5 12.6 2.6
FX 84-W-218 21.9 3.2 1.719 35.0 -0.5 9.9 5.0
GOE 477 AIRFOIL 10.0 4.9 1.653 76.3 -0.5 12.4 3.0
FX 84-W-175 17.6 4.4 1.763 43.4 -0.5 8.6 3.4
GOE 476 AIRFOIL 14.4 5.2 1.764 50.0 -0.5 20.5 4.5