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
NASA SC(2)-0503 AIRFOIL 3.0 0.2 0.435 23.9 4.5 6.5 1.3
NASA SC(2)-0403 AIRFOIL 3.0 0.4 0.408 19.4 5.0 6.3 1.3
GOE 451 AIRFOIL 4.4 5.5 1.244 338.2 -0.5 6.1 1.4
GOE 9K AIRFOIL 2.4 0.9 0.611 71.3 4.5 7.3 1.4
GOE 5K AIRFOIL 3.7 1.5 0.726 76.1 5.0 10.6 1.4
NASA SC(2)-0404 AIRFOIL 4.0 0.5 0.495 18.5 6.0 7.4 1.4
YS-900 9.0 0.0 0.311 11.6 5.5 19.8 1.5
NACA 66-206 6.0 1.1 0.620 26.8 8.0 6.0 1.5
NACA 65-206 6.0 1.1 0.627 26.3 1.0 4.5 1.5
GOE 559 AIRFOIL 11.1 3.4 0.883 59.9 3.5 14.2 1.5
GOE 443 AIRFOIL 5.0 0.0 0.512 30.1 3.0 7.4 1.5
NACA 64-206 6.0 1.1 0.639 26.8 0.5 3.6 1.5
FX 74-080 8.1 4.3 1.010 57.7 -0.5 10.5 1.5
NACA 63-206 6.0 1.1 0.539 19.0 -0.5 3.2 1.5
GOE 419 AIRFOIL 5.3 4.4 0.981 72.5 3.5 11.8 1.5
NACA 16-006 6.0 0.0 0.524 23.3 2.5 17.4 1.5
GOE 444 AIRFOIL 5.6 0.0 0.515 31.6 3.5 10.3 1.5
GOE 10K AIRFOIL 3.8 1.4 0.736 68.0 3.5 11.5 1.6
E63 (4.25%) 4.3 5.4 1.353 122.3 4.0 6.1 1.6
dh4009sm 8.9 0.2 0.674 27.7 2.0 22.1 1.6
BOEING-VERTOL VR-9 AIRFOIL 6.0 0.3 0.540 15.8 9.5 6.3 1.6
GOE 587 AIRFOIL 5.8 3.0 0.844 38.1 2.0 10.8 1.6
GOE 590 AIRFOIL 5.7 4.0 0.902 61.2 4.0 10.3 1.6
FX 66-H-60 6.0 1.7 0.572 40.3 4.5 7.2 1.6
EPPLER 908 AIRFOIL 9.0 2.8 0.782 52.8 -0.5 13.8 1.6
EPPLER 904 AIRFOIL 9.0 1.3 0.577 42.1 2.5 14.1 1.6
GOE 391 AIRFOIL 5.1 3.2 0.983 56.0 2.0 11.3 1.6
NASA SC(2)-0706 AIRFOIL 6.0 0.4 0.819 30.3 0.5 9.4 1.6
E71 (5.15%) 5.2 4.6 1.208 136.6 4.0 3.7 1.6
NASA SC(2)-1006 AIRFOIL 6.0 0.0 0.930 77.3 -0.5 9.5 1.6
HQ 0/7 AIRFOIL 7.0 0.0 0.475 29.5 3.0 5.0 1.6
YS-915 9.1 1.8 0.612 34.0 -0.5 15.0 1.6
NASA SC(2)-0606 AIRFOIL 6.0 0.4 0.766 26.0 1.0 10.3 1.6
NACA 16009 9.0 0.0 0.537 23.3 3.0 26.4 1.6
Eh 1.0/7.0 7.0 1.0 0.567 41.2 3.5 5.7 1.6
EH 2.0/7.0 7.0 2.0 0.635 54.8 4.5 5.7 1.6
ONERA OA206 AIRFOIL 6.0 0.8 0.643 31.2 4.5 7.1 1.6
GOE 445 AIRFOIL 6.4 0.0 0.552 40.2 4.0 10.3 1.6
NASA SC(2)-0406 AIRFOIL 6.0 0.3 0.664 21.6 2.0 10.4 1.6
AG47ct -02f rot. 5.0 1.3 0.756 43.2 5.5 5.6 1.6
AG47c -03f 5.0 2.0 0.759 44.1 6.5 4.9 1.7
MH 121 8.76% 8.8 3.0 0.878 82.5 3.0 9.7 1.7
HT08 5.0 0.0 0.581 19.3 3.0 12.7 1.7
E62 (5.62%) 5.6 5.4 1.319 106.2 4.5 6.5 1.7
GOE 370 AIRFOIL 4.6 5.7 1.157 79.5 4.5 10.1 1.7
GOE 427 AIRFOIL 4.6 5.7 1.206 60.0 1.5 9.5 1.7
EPPLER E851 AIRFOIL 9.0 2.4 0.763 57.2 2.5 10.3 1.7
EPPLER 818 HYDROFOIL AIRFOIL 9.3 2.8 0.767 65.4 1.0 6.9 1.7
EPPLER 874 HYDROFOIL AIRFOIL 7.9 1.0 0.547 33.1 3.0 15.1 1.7