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 (%)
E423 12.5 10.0 2.357 67.7 14.5 14.1 3.2
EPPLER 338 AIRFOIL 13.3 3.7 1.283 44.3 14.5 14.3 2.5
GOE 404 AIRFOIL 13.1 5.0 1.655 48.6 14.5 18.5 4.5
GOE 367 AIRFOIL 16.3 4.6 1.749 42.5 14.5 28.9 4.1
EPPLER 856 AIRFOIL 18.1 4.3 1.762 62.0 14.5 18.6 3.1
EPPLER 639 AIRFOIL 12.5 4.8 1.375 43.1 14.5 15.0 2.6
EPPLER 638 AIRFOIL 12.3 4.4 1.287 38.3 14.5 15.0 2.6
EPPLER 560 AIRFOIL 16.1 4.9 1.827 76.0 14.5 12.7 3.5
EPPLER 558 AIRFOIL 16.0 3.6 1.605 63.8 14.5 14.1 3.6
GOE 530 AIRFOIL 12.8 5.1 1.556 48.3 14.5 20.3 4.1
GOE 498 AIRFOIL 15.9 5.5 1.904 59.8 14.0 14.3 4.7
NASA/LANGLEY NLF(1)-0416 AIRFOIL 15.9 2.5 1.528 67.6 14.0 8.7 2.9
NACA 4415 15.0 4.0 1.643 55.4 14.0 24.3 3.4
DAVIS BASIC B-24 WING AIRFOIL 15.9 2.5 1.224 27.1 14.0 15.1 3.3
CLARK YM-15 AIRFOIL 14.9 3.5 1.597 60.0 14.0 23.1 4.1
GOE 758 AIRFOIL 13.8 4.7 1.619 53.1 14.0 14.1 3.2
S8037 (16%) 16.0 2.6 1.389 42.0 14.0 23.7 2.9
BOEING 707 .40 SPAN AIRFOIL 9.6 1.9 0.997 41.4 14.0 11.6 1.9
EPPLER 637 AIRFOIL 12.1 3.5 1.182 33.6 14.0 14.9 2.4
EPPLER 635 AIRFOIL 11.6 2.9 0.964 22.9 14.0 14.9 2.5
EPPLER 625 AIRFOIL 13.0 2.9 1.152 35.3 14.0 17.3 2.8
EPPLER 559 AIRFOIL 16.0 4.2 1.720 69.7 14.0 12.7 3.5
GOE 553 AIRFOIL 13.6 4.6 1.697 54.7 14.0 10.5 3.6
GOE 528 AIRFOIL 12.4 6.1 1.820 57.9 14.0 14.4 3.3
GOE 510 AIRFOIL 13.7 5.8 1.773 68.1 14.0 24.7 4.0
GOE 460 AIRFOIL 20.4 0.0 1.215 33.6 13.5 25.9 5.1
EPPLER 337 AIRFOIL 13.1 3.2 1.165 38.3 13.5 14.4 2.4
EPPLER 329 AIRFOIL 13.5 3.5 1.306 54.9 13.5 13.6 2.5
TRAINER60 18.3 0.2 1.064 24.3 13.5 52.5 4.2
GOE 412 AIRFOIL 13.1 5.1 1.743 51.9 13.5 25.0 3.3
GOE 364 AIRFOIL 10.7 6.5 1.781 67.0 13.5 14.5 3.2
GOE 29B AIRFOIL 9.4 6.5 1.700 50.9 13.5 14.9 3.5
GOE 298 AIRFOIL 12.8 4.5 1.539 38.9 13.5 23.3 4.7
EPPLER 636 AIRFOIL 11.9 3.1 1.055 27.9 13.5 15.0 2.4
MH 104 15.28% 15.2 2.0 1.101 25.8 13.5 12.3 2.7
GOE 478 AIRFOIL 13.3 4.3 1.628 55.4 13.0 17.7 4.0
EPPLER 335 AIRFOIL 12.6 2.4 0.952 28.4 13.0 14.3 2.3
EPPLER 334 AIRFOIL 11.9 4.0 1.292 53.2 13.0 12.8 2.3
HQ 3.0/15 AIRFOIL 15.0 3.0 1.526 53.7 13.0 11.1 3.0
SM701 16.0 3.3 1.712 56.4 13.0 9.1 3.3
NACA 6412 12.0 6.0 1.622 55.6 13.0 21.3 3.0
GOE 615 AIRFOIL 13.6 5.6 1.771 60.7 13.0 16.5 4.0
GOE 15 AIRFOIL 9.0 7.7 1.844 72.5 13.0 15.2 3.2
EPPLER 432 AIRFOIL 15.9 4.4 1.663 54.5 13.0 10.7 2.6
EPPLER 333 AIRFOIL 11.7 3.6 1.179 48.6 12.5 13.0 2.3
EPPLER 327 AIRFOIL 13.1 2.6 1.094 41.6 12.5 13.2 2.4
EPPLER 326 AIRFOIL 12.8 2.2 0.989 41.9 12.5 13.2 2.3
GOE 426 AIRFOIL 13.5 4.5 1.571 53.0 12.5 10.1 3.1
GOE 418 AIRFOIL 12.7 5.0 1.545 51.7 12.5 13.5 4.4
SPICA 11.73% smoothed 11.7 4.7 1.530 54.9 12.5 14.4 2.9