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 (%)
NASA SC(2)-0402 AIRFOIL 2.0 0.2 0.328 20.2 3.5 5.1 1.3
EPPLER 379 AIRFOIL 2.2 8.0 0.545 73.3 -0.5 2.8 1.7
EPPLER 376 AIRFOIL 2.4 8.9 1.441 132.7 4.0 2.4 1.7
GOE 9K AIRFOIL 2.4 0.9 0.611 71.3 4.5 7.3 1.4
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil 2.7 6.2 0.760 36.6 -0.5 16.2 1.7
NASA SC(2)-0403 AIRFOIL 3.0 0.4 0.408 19.4 5.0 6.3 1.3
NASA SC(2)-0503 AIRFOIL 3.0 0.2 0.435 23.9 4.5 6.5 1.3
GOE 417A (GEW. PLATTE) AIRFOIL 3.1 5.9 1.230 76.8 2.5 14.4 1.8
GOE 5K AIRFOIL 3.7 1.5 0.726 76.1 5.0 10.6 1.4
EPPLER 377 (MODIFIED) AIRFOIL 3.7 9.1 1.453 103.6 9.5 3.3 1.8
EPPLER 377 AIRFOIL 3.8 8.7 1.609 127.2 7.0 2.8 1.8
GOE 10K AIRFOIL 3.8 1.4 0.736 68.0 3.5 11.5 1.6
NASA SC(2)-0404 AIRFOIL 4.0 0.5 0.495 18.5 6.0 7.4 1.4
EPPLER 378 AIRFOIL 4.0 8.0 1.183 16.7 -0.5 2.8 1.8
E63 (4.25%) 4.3 5.4 1.353 122.3 4.0 6.1 1.6
GOE 451 AIRFOIL 4.4 5.5 1.244 338.2 -0.5 6.1 1.4
GOE 427 AIRFOIL 4.6 5.7 1.206 60.0 1.5 9.5 1.7
GOE 370 AIRFOIL 4.6 5.7 1.157 79.5 4.5 10.1 1.7
GOE 396 AIRFOIL 4.7 5.7 1.347 71.8 5.5 10.1 1.7
AG10 4.7 1.7 0.772 35.3 5.0 12.4 1.7
HT05 4.8 0.0 0.590 18.0 2.5 16.8 1.7
AG09 4.8 1.9 0.743 40.4 5.0 9.0 1.7
GOE 491 AIRFOIL 4.8 2.9 0.924 44.7 3.0 12.5 1.8
Bergey BW-3 (smoothed) 4.9 5.8 1.282 50.6 4.0 49.0 2.1
GOE 494 AIRFOIL 4.9 5.1 1.144 76.7 -0.5 5.5 1.7
AG47ct -02f rot. 5.0 1.3 0.756 43.2 5.5 5.6 1.6
HT08 5.0 0.0 0.581 19.3 3.0 12.7 1.7
GOE 443 AIRFOIL 5.0 0.0 0.512 30.1 3.0 7.4 1.5
HT12 5.0 0.0 0.588 23.8 3.5 8.9 1.7
AG47c -03f 5.0 2.0 0.759 44.1 6.5 4.9 1.7
S1091 5.1 6.1 1.544 90.2 8.0 10.2 1.9
HT22 5.1 1.1 0.766 37.8 5.0 7.6 1.7
GOE 397 AIRFOIL 5.1 3.9 1.011 68.6 5.0 8.5 1.7
GOE 391 AIRFOIL 5.1 3.2 0.983 56.0 2.0 11.3 1.6
E71 (5.15%) 5.2 4.6 1.208 136.6 4.0 3.7 1.6
GOE 419 AIRFOIL 5.3 4.4 0.981 72.5 3.5 11.8 1.5
AG14 5.4 2.1 0.920 48.3 6.0 6.0 1.7
GOE 342 AIRFOIL 5.4 6.2 1.708 70.7 1.0 12.9 2.0
GOE 123 AIRFOIL 5.4 5.7 1.349 71.8 3.0 12.5 2.0
AG19 5.4 2.3 0.941 48.5 6.0 6.0 1.7
GOE 483 AIRFOIL 5.4 5.8 1.409 83.3 8.0 6.2 1.8
GOE 444 AIRFOIL 5.6 0.0 0.515 31.6 3.5 10.3 1.5
EPPLER 59 AIRFOIL 5.6 5.2 1.386 81.5 0.5 6.3 1.8
EPPLER 58 AIRFOIL 5.6 6.4 1.808 84.9 -0.5 5.1 1.8
E62 (5.62%) 5.6 5.4 1.319 106.2 4.5 6.5 1.7
Coanda 1 5.6 4.2 0.874 72.8 5.5 18.7 1.9
E61 (5.64%) 5.7 6.7 1.577 89.1 5.0 6.4 1.7
GOE 590 AIRFOIL 5.7 4.0 0.902 61.2 4.0 10.3 1.6
GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL 5.7 3.8 1.132 56.9 3.5 16.9 1.9
GOE 587 AIRFOIL 5.8 3.0 0.844 38.1 2.0 10.8 1.6