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 : 1765 (showing the first 50)

Name Thickness (%) Camber (%) Lift Coeff. (CL) Lift-to-Drag (L/D) Stall Angle (deg) TE Angle (deg) LE Radius (%)
NASA SC(2)-0402 2.0 0.2 0.328 15.7 3.5 6.2 0.4
EPPLER 379 2.1 8.0 0.545 57.7 -0.5 2.5 1.2
EPPLER 376 2.3 8.9 1.441 133.7 4.0 2.4 1.1
GOE 9K 2.5 0.9 0.612 59.1 4.5 3.4 3.8
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil 2.6 6.2 0.760 31.6 -0.5 1.5 2.3
Eiffel 10 (Wright) - 1903 Wright Flyer 2.6 6.2 0.760 31.6 -0.5 5.2 2.2
NASA SC(2)-0403 3.0 0.4 0.408 16.0 5.0 7.3 0.5
NASA SC(2)-0503 3.0 0.2 0.435 18.1 4.5 1.5 0.5
GOE 417A (GEW. PLATTE) 3.2 5.9 1.231 65.4 2.5 3.3 2.5
EPPLER 377 3.7 8.7 1.610 181.2 7.0 2.7 1.3
GOE 5K 3.7 1.5 0.727 64.5 5.0 5.1 2.9
EPPLER 377 (MODIFIED) 3.8 9.1 1.463 60.8 9.5 3.2 1.3
GOE 10K 3.9 1.4 0.736 57.1 3.5 5.3 3.9
EPPLER 378 3.9 8.0 1.183 8.7 -0.5 2.7 1.4
KFm3-TGK 4.0 4.0 1.600 180.4 -5.0 76.1 10.1
NASA SC(2)-0404 4.0 0.5 0.495 15.1 0.5 8.6 0.6
E63 (4.25%) 4.3 5.4 1.354 83.5 4.0 5.8 1.4
E63 (4.25%) 4.3 5.4 1.354 83.5 4.0 6.6 1.4
GOE 451 4.4 5.6 1.245 250.3 -0.5 7.0 2.5
GOE 427 4.6 5.7 1.206 50.8 1.5 5.4 2.3
GOE 370 4.7 5.7 1.158 70.7 4.5 5.6 2.3
GOE 396 4.7 5.8 1.348 62.5 5.5 5.6 2.4
AG10 4.7 1.7 0.772 20.8 5.0 4.2 0.8
Bergey BW-3 (smoothed) 4.8 5.8 1.282 32.2 4.0 79.7 1.6
HT05 4.8 0.0 0.590 12.6 3.0 20.7 0.6
GOE 491 4.8 2.9 0.924 43.4 3.0 5.9 2.4
AG09 4.9 1.9 0.743 24.9 5.0 4.5 0.6
GOE 494 5.0 5.1 1.145 61.2 -0.5 4.6 2.3
AG47ct-02f rot. 5.0 1.3 0.756 25.8 5.5 4.1 0.5
HT08 5.0 0.0 0.581 11.9 3.0 16.3 0.6
GOE 443 5.0 0.0 0.512 24.3 3.0 6.6 2.1
Bergey BW-3 (smoothed) 5.0 5.8 1.282 32.2 4.0 19.3 1.6
HT12 5.0 0.0 0.588 12.1 3.5 3.5 0.6
S1091 5.1 6.1 1.544 70.1 8.0 9.6 1.2
AG47c-03f 5.1 2.0 0.759 26.5 6.5 3.5 0.5
HT22 5.1 1.1 0.766 22.7 5.0 3.9 0.8
GOE 391 5.1 3.2 0.983 47.1 2.0 10.7 2.2
GOE 397 5.1 4.0 1.012 57.5 5.0 5.8 2.3
E71 (5.15%) 5.2 4.6 1.209 111.5 4.0 2.7 1.3
E71 (5.15%) 5.2 4.6 1.209 111.5 4.0 5.6 1.3
GOE 419 5.3 4.4 0.982 60.0 3.5 6.5 2.2
AG14 5.4 2.1 0.920 32.1 6.0 3.7 0.5
GOE 123 5.4 5.7 1.350 57.0 3.0 5.8 2.6
GOE 342 5.4 6.2 1.710 56.7 1.0 5.0 2.6
AG19 5.4 2.3 0.941 33.1 6.0 3.7 0.5
GOE 483 5.5 5.8 1.410 69.6 8.0 5.5 2.5
EPPLER 58 5.6 6.5 1.810 68.4 -0.5 6.0 2.5
GOE 444 5.6 0.0 0.515 31.8 3.5 9.1 2.1
EPPLER 59 5.6 5.2 1.388 73.3 0.5 5.9 2.4
E62 (5.62%) 5.6 5.4 1.319 71.1 4.5 5.3 1.4