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 (%)
FX 79-W-660A 66.4 2.3 2.013 11.2 2.0 158.2 20.1
FX 69-PR-281 28.1 5.6 2.154 39.2 -0.5 16.1 12.3
FX 79-W-470A 46.3 3.8 1.727 11.0 1.0 148.6 12.2
EPPLER 864 STRUT AIRFOIL 38.8 0.0 1.384 13.8 3.0 61.4 10.9
AH 93-W-300 30.0 1.1 1.516 17.8 -0.5 48.4 10.8
GOE 570 AIRFOIL 33.6 9.6 2.416 42.5 -0.5 49.2 10.7
EPPLER 863 STRUT AIRFOIL 35.7 0.0 1.326 14.2 2.5 55.0 9.8
WORTMANN FX 77-W-343 AIRFOIL 34.2 4.7 1.374 9.4 -0.5 73.1 9.3
GOE 435 AIRFOIL 26.0 4.7 2.037 33.4 -0.5 21.4 9.1
KENNEDY AND MARSDEN AIRFOIL 27.9 7.7 2.646 55.4 -0.5 8.6 9.1
Marsden 27.8 9.6 2.809 59.3 -5.5 8.6 8.8
EPPLER 862 STRUT AIRFOIL 32.3 0.0 1.318 14.8 2.0 48.0 8.7
GOE 434 AIRFOIL 22.7 5.1 2.042 38.8 -0.5 18.7 8.2
GOE 561 AIRFOIL 24.9 10.2 2.234 40.5 -0.5 42.7 7.9
RAF 89 AIRFOIL 24.8 1.6 1.582 30.7 -0.5 26.8 7.9
NACA 23024 23.9 1.9 1.360 29.9 1.5 35.8 7.8
GOE 571 AIRFOIL 24.8 9.8 2.248 40.0 -0.5 38.6 7.6
NACA 2424 23.9 2.0 1.580 37.0 0.5 35.7 7.5
GOE 776 AIRFOIL 24.9 0.3 1.297 24.3 2.5 42.0 7.5
AH 94-W-301 30.1 1.1 1.442 17.1 -0.5 53.4 7.3
NACA 0024 23.9 0.0 1.284 25.3 3.0 40.6 7.1
AH 81-K-144 W-F KLAPPE 21.7 1.1 1.064 11.4 2.0 24.9 6.8
GOE 386 AIRFOIL 20.1 5.4 1.924 38.4 -0.5 29.7 6.8
GOE 522 AIRFOIL 21.7 5.2 2.060 47.1 -0.5 21.0 6.7
GOE 390 AIRFOIL 20.1 6.9 2.126 40.6 -0.5 27.1 6.7
GOE 652 AIRFOIL 16.9 9.2 2.483 61.3 -0.5 4.0 6.4
GOE 244 (MVA PR.4) AIRFOIL 17.6 9.9 2.694 54.4 -0.5 11.4 6.2
RAF 69 AIRFOIL 20.5 1.7 1.531 37.1 1.5 22.1 6.2
FX 77-W-270S 27.0 4.3 1.265 13.1 0.0 54.7 6.1
FX 77-W-270 27.0 4.3 0.283 2.1 -0.5 70.7 6.1
GOE 625 AIRFOIL 19.9 6.2 2.037 34.8 -0.5 37.5 6.1
WORTMANN FX 77-W-258 AIRFOIL 26.1 4.3 1.652 15.8 -0.5 37.9 6.0
GOE 798 AIRFOIL 20.0 6.2 2.164 47.2 1.0 42.4 6.0
GOE 243 (MVA PR.3) AIRFOIL 18.9 8.4 2.458 56.0 -0.5 13.6 6.0
GOE 217 (MVA MK.12) AIRFOIL 18.9 6.3 2.134 38.5 -0.5 25.5 6.0
GOE 777 AIRFOIL 21.9 5.9 1.789 29.4 -0.5 27.4 6.0
USA 35 AIRFOIL 18.0 6.4 2.020 41.2 -0.5 28.9 6.0
USA 35 A AIRFOIL 18.0 6.4 2.018 41.0 -0.5 28.9 5.9
FX 69-274 27.4 3.2 1.342 21.9 1.5 47.3 5.9
GOE 775 AIRFOIL 20.9 0.2 1.195 28.5 4.5 36.1 5.9
NACA 0021 20.9 0.0 1.197 28.3 4.5 35.9 5.9
GOE 679 AIRFOIL 18.2 4.5 1.878 71.5 5.5 26.5 5.9
GOE 735 AIRFOIL 19.9 4.3 1.405 20.5 -0.5 17.4 5.8
GOE 383 AIRFOIL 20.1 5.0 1.808 33.8 -0.5 28.0 5.8
ARA-D 20% AIRFOIL 20.0 3.7 1.539 14.5 1.5 56.5 5.7
USA 34 AIRFOIL 17.9 7.7 2.223 49.0 -0.5 30.9 5.7
GOE 382 AIRFOIL 19.9 6.0 1.954 36.4 -0.5 25.7 5.6
GOE 241 (MVA PR.1) AIRFOIL 18.7 8.4 2.477 54.1 -0.5 18.7 5.5
GOE 481A AIRFOIL 15.2 5.5 2.011 79.2 9.0 30.5 5.5
NASA/LANGLEY LS(1)-0421MOD AIRFOIL 20.9 2.1 1.759 33.4 -0.6 25.4 5.4