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 (%)
GOE 462 AIRFOIL 10.8 13.3 2.381 596.0 0.0 4.7 3.7
GOE 481 AIRFOIL 12.8 8.8 2.295 421.1 10.0 23.1 5.4
GOE 464 AIRFOIL 7.5 9.9 2.099 392.6 0.0 9.3 3.3
GOE 451 AIRFOIL 4.4 5.5 1.244 338.2 -0.5 6.1 1.4
FX 60-100 AIRFOIL 10.0 3.6 1.366 323.8 7.5 3.3 2.1
KFm3-TGK 11.3 5.7 1.598 316.5 -5.0 58.0 2.1
GOE 531 AIRFOIL 13.7 14.5 2.796 290.9 -0.5 21.9 5.3
KFm2-TGK 8.8 4.4 1.502 281.2 -5.0 58.0 2.0
SARATOV AIRFOIL 9.2 9.6 1.762 192.0 0.0 8.8 3.0
WORTMANN FX 082-512 AIRFOIL 11.6 4.1 1.440 164.0 3.5 10.3 2.7
GOE 369 AIRFOIL 5.8 5.4 1.393 161.1 0.0 8.5 1.9
WORTMANN FX 60-126 AIRFOIL 12.5 3.6 1.491 145.5 10.0 4.1 2.6
GOE 802 B AIRFOIL 9.8 6.1 1.739 141.7 2.0 20.9 3.0
S1223 RTL 13.5 8.5 2.264 140.7 5.0 10.8 3.2
E71 (5.15%) 5.2 4.6 1.208 136.6 4.0 3.7 1.6
EPPLER 376 AIRFOIL 2.4 8.9 1.441 132.7 4.0 2.4 1.7
EPPLER 377 AIRFOIL 3.8 8.7 1.609 127.2 7.0 2.8 1.8
E385 (8.41%) 8.4 5.7 1.491 126.2 7.0 3.5 1.9
S1223 12.1 8.7 2.425 125.4 8.0 9.0 3.2
E63 (4.25%) 4.3 5.4 1.353 122.3 4.0 6.1 1.6
FX 61-147 AIRFOIL 14.7 3.2 1.679 117.5 7.5 9.7 2.4
EPPLER 664 (EXTENDED) AIRFOIL 16.6 2.8 2.433 117.4 -0.5 10.2 2.6
GOE 440 AIRFOIL 15.2 9.7 1.864 117.3 0.5 12.7 2.0
E471 (6.25%) 6.3 4.7 1.287 111.9 5.0 4.8 1.7
E216 (10.4%) 10.4 5.2 1.805 110.8 8.5 8.7 2.2
S1210 12% 12.0 7.2 2.248 109.9 9.0 4.8 2.7
FX 60-177 AIRFOIL 17.7 2.7 1.114 108.4 3.0 9.3 3.1
FX 61-163 AIRFOIL 16.3 2.6 1.435 107.1 5.5 7.0 2.5
MH 115 11.06% 11.1 5.6 1.725 107.0 7.0 8.4 2.3
EPPLER 395 AIRFOIL 12.3 5.2 1.589 106.9 8.0 8.7 2.4
E62 (5.62%) 5.6 5.4 1.319 106.2 4.5 6.5 1.7
FX 61-140 AIRFOIL 13.9 2.5 1.422 105.9 6.5 5.4 2.2
MH 38 9.68% 9.7 3.9 1.100 105.4 5.5 5.7 1.9
EPPLER EC 86(-3)-914 AIRFOIL 14.3 4.4 1.785 103.8 -0.5 4.2 2.5
EPPLER 377 (MODIFIED) AIRFOIL 3.7 9.1 1.453 103.6 9.5 3.3 1.8
MH 116 9.84% 9.8 4.1 1.316 99.5 6.5 8.5 2.0
Eiffel 428 (Bleriot) 8.9 5.1 1.189 98.0 -0.5 13.0 2.2
FX 63-137 13.7% smoothed 13.7 6.0 2.037 97.9 12.0 5.5 3.0
GOE 802 A AIRFOIL 9.8 6.1 1.742 96.3 8.0 20.9 3.0
FX 61-168 AIRFOIL 16.8 3.0 1.573 96.3 6.0 9.6 2.6
FX 63-145 AIRFOIL 14.5 4.0 1.538 95.4 -0.5 6.6 2.7
RAE(NPL) 5213 AIRFOIL 9.9 1.4 1.149 95.0 6.0 6.5 2.4
RAE 5214 AIRFOIL 9.7 1.4 1.142 94.9 6.0 6.5 2.4
FX 80-080 8.1 2.2 0.979 94.6 4.0 11.8 1.7
S4022 11.2 4.3 1.599 94.3 8.0 10.6 2.1
GOE 380 AIRFOIL 6.5 5.6 1.474 91.9 7.5 11.8 1.9
WORTMANN FX 63-137 AIRFOIL 13.7 6.0 2.013 91.7 7.5 5.0 3.0
GOE 275 (DAIMLER VI) AIRFOIL 7.7 4.7 1.528 91.5 8.0 11.8 2.3
S1091 5.1 6.1 1.544 90.2 8.0 10.2 1.9
RAF 19 AIRFOIL 10.4 10.1 2.050 89.7 5.0 19.6 3.8