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 (%)
STRAND AIRFOIL 15.4 4.0 1.448 19.0 -0.5 0.3 3.3
MH 150 23.89% 23.9 5.4 2.056 41.4 -0.5 0.7 5.2
MH 83 13.29% 13.3 5.1 1.478 40.1 -0.4 1.8 3.3
WORTMANN FX 62-K-131 AIRFOIL 13.1 3.9 1.474 35.2 5.5 2.1 2.0
EPPLER 376 AIRFOIL 2.4 8.9 1.441 132.7 4.0 2.4 1.7
S4180-098-84 9.8 4.4 1.388 59.0 11.5 2.4 2.6
EPPLER 378 AIRFOIL 4.0 8.0 1.183 16.7 -0.5 2.8 1.8
EPPLER 379 AIRFOIL 2.2 8.0 0.545 73.3 -0.5 2.8 1.7
EPPLER 377 AIRFOIL 3.8 8.7 1.609 127.2 7.0 2.8 1.8
WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL 11.0 2.3 1.209 45.5 -0.5 2.9 3.0
NACA 63-206 6.0 1.1 0.539 19.0 -0.5 3.2 1.5
DSMA-523A AIRFOIL 11.0 2.3 1.282 39.7 1.5 3.2 2.9
FX 60-100 AIRFOIL 10.0 3.6 1.366 323.8 7.5 3.3 2.1
EPPLER 377 (MODIFIED) AIRFOIL 3.7 9.1 1.453 103.6 9.5 3.3 1.8
FX60-100 10.0% smoothed 9.9 3.5 1.387 51.1 8.5 3.4 2.1
E385 (8.41%) 8.4 5.7 1.491 126.2 7.0 3.5 1.9
NACA 64-206 6.0 1.1 0.639 26.8 0.5 3.6 1.5
E71 (5.15%) 5.2 4.6 1.208 136.6 4.0 3.7 1.6
S6063 7.05% 6.9 1.4 0.733 45.6 4.0 4.0 1.8
SD5060 (9.5%) 9.5 2.3 1.102 52.8 9.0 4.0 2.3
GOE 652 AIRFOIL 16.9 9.2 2.483 61.3 -0.5 4.0 6.4
FX 63-100 AIRFOIL 9.9 4.3 1.556 80.6 7.0 4.0 2.4
WORTMANN FX 60-126 AIRFOIL 12.5 3.6 1.491 145.5 10.0 4.1 2.6
LNV109A 13.0 5.9 1.505 21.6 -0.5 4.1 4.0
SD7043 (9.1%) 9.1 3.5 1.342 71.3 9.5 4.1 2.3
S4061-096-84 9.6 3.9 1.292 59.4 9.5 4.2 2.1
FX 60-100 (126) AIRFOIL 10.1 3.6 1.418 68.6 7.5 4.2 2.3
S5020 8.4 2.6 0.939 68.1 10.0 4.2 2.0
EPPLER EC 86(-3)-914 AIRFOIL 14.3 4.4 1.785 103.8 -0.5 4.2 2.5
S3010-103-84 10.3 2.8 1.190 53.8 10.0 4.3 2.3
S2091-101-83 10.1 3.9 1.348 57.4 11.0 4.3 2.5
FX 84-W-097 9.7 2.8 1.004 53.1 7.0 4.4 2.0
NACA 65-206 6.0 1.1 0.627 26.3 1.0 4.5 1.5
FX 63-110 AIRFOIL 11.0 4.3 1.578 84.1 6.5 4.5 2.7
NACA 63-209 9.0 1.1 0.830 36.3 2.5 4.5 1.9
S2046 9.0 2.6 1.224 77.9 7.5 4.6 2.1
SD7034 10.5 3.9 1.358 56.6 11.5 4.6 2.6
SELIG 3002-099-83 9.9 3.0 1.325 68.0 9.5 4.6 2.2
NACA 63-210 AIRFOIL 10.0 1.1 0.899 23.7 1.0 4.7 2.0
S6062 8% 7.9 1.6 0.813 53.8 5.0 4.7 1.9
MH 62 9.3% 9.3 1.6 0.871 67.9 8.0 4.7 2.0
NACA 64-208 8.0 1.1 0.757 33.4 2.0 4.7 1.7
GOE 462 AIRFOIL 10.8 13.3 2.381 596.0 0.0 4.7 3.7
NACA 64-108 AIRFOIL 8.0 0.6 0.678 21.7 1.5 4.7 1.7
FX 63-120 AIRFOIL 12.0 5.2 1.963 87.4 9.0 4.7 2.9
E471 (6.25%) 6.3 4.7 1.287 111.9 5.0 4.8 1.7
S1210 12% 12.0 7.2 2.248 109.9 9.0 4.8 2.7
EPPLER EA 6(-1)-009 AIRFOIL 9.0 0.0 0.869 36.5 4.5 4.8 2.3
WORTMANN FX 72-MS-150B AIRFOIL 15.0 9.7 2.116 38.9 11.0 4.8 2.6
MH 45 9.85% 9.8 1.7 0.888 66.7 6.5 4.8 2.1