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 79-W-470A 46.3 3.8 1.727 11.0 1.0 148.6 12.2
SIKORSKY DBLN-526 AIRFOIL 25.9 4.0 2.240 57.9 -0.5 113.0 5.1
WORTMANN FX 77-W-343 AIRFOIL 34.2 4.7 1.374 9.4 -0.5 73.1 9.3
FX 77-W-270 27.0 4.3 0.283 2.1 -0.5 70.7 6.1
EPPLER 864 STRUT AIRFOIL 38.8 0.0 1.384 13.8 3.0 61.4 10.9
KFm3-TGK 11.3 5.7 1.598 316.5 -5.0 58.0 2.1
KFm2-TGK 8.8 4.4 1.502 281.2 -5.0 58.0 2.0
ARA-D 20% AIRFOIL 20.0 3.7 1.539 14.5 1.5 56.5 5.7
GOE 16K AIRFOIL 18.1 4.1 1.789 46.9 -0.5 56.5 4.4
NACA 16-021 20.9 0.0 1.142 32.8 0.5 56.2 3.8
EPPLER 863 STRUT AIRFOIL 35.7 0.0 1.326 14.2 2.5 55.0 9.8
FX 77-W-270S 27.0 4.3 1.265 13.1 0.0 54.7 6.1
AH 94-W-301 30.1 1.1 1.442 17.1 -0.5 53.4 7.3
TRAINER60 18.3 0.2 1.064 24.3 13.5 52.5 4.2
GOE 711 AIRFOIL 14.8 6.5 1.929 46.8 7.5 49.4 3.3
NACA 16-018 17.9 0.0 1.068 33.5 0.5 49.3 3.2
GOE 570 AIRFOIL 33.6 9.6 2.416 42.5 -0.5 49.2 10.7
Bergey BW-3 (smoothed) 4.9 5.8 1.282 50.6 4.0 49.0 2.1
AH 93-W-300 30.0 1.1 1.516 17.8 -0.5 48.4 10.8
EPPLER 862 STRUT AIRFOIL 32.3 0.0 1.318 14.8 2.0 48.0 8.7
GOE 15K AIRFOIL 14.9 3.4 1.517 67.9 -0.5 48.0 3.6
FX 69-274 27.4 3.2 1.342 21.9 1.5 47.3 5.9
ARA-D 13% AIRFOIL 13.0 3.6 1.421 28.4 -0.7 46.5 3.8
GOE 575 AIRFOIL 13.3 3.6 1.744 60.6 10.5 46.3 3.9
Glenn Martin 3 13.7 6.9 1.696 60.5 8.5 45.3 3.7
Glenn Martin 4 15.5 7.7 2.371 74.4 10.5 44.7 3.4
NACA 23021 21.0 2.4 0.443 6.6 7.5 44.5 4.9
GOE 561 AIRFOIL 24.9 10.2 2.234 40.5 -0.5 42.7 7.9
NACA 2421 21.0 2.0 0.501 7.3 7.5 42.4 4.7
GOE 798 AIRFOIL 20.0 6.2 2.164 47.2 1.0 42.4 6.0
GOE 776 AIRFOIL 24.9 0.3 1.297 24.3 2.5 42.0 7.5
NACA 16-015 14.9 0.0 0.956 29.8 5.0 41.9 2.7
ARA-D 10% AIRFOIL 10.0 4.0 1.432 38.8 9.5 41.6 3.0
davissm 5.9 5.9 1.324 50.3 5.5 41.0 1.7
USNPS4 (smoothed) 11.9 5.0 1.727 48.1 10.5 40.6 2.6
NACA 0024 23.9 0.0 1.284 25.3 3.0 40.6 7.1
GOE 13K AIRFOIL 14.8 5.4 1.876 83.4 -0.5 40.1 4.3
GOE 14K AIRFOIL 12.0 2.7 1.210 64.6 0.5 39.3 2.9
GOE 8K AIRFOIL 14.8 6.1 1.880 74.1 -0.5 38.8 3.1
NACA 0010-66 10.0 0.0 0.857 28.6 4.0 38.7 2.4
GOE 571 AIRFOIL 24.8 9.8 2.248 40.0 -0.5 38.6 7.6
NACA 23018 18.0 2.0 1.035 20.7 -0.5 38.3 4.0
WORTMANN FX 77-W-258 AIRFOIL 26.1 4.3 1.652 15.8 -0.5 37.9 6.0
Falcon 13.7 1.6 1.124 44.1 10.5 37.8 2.7
GOE 625 AIRFOIL 19.9 6.2 2.037 34.8 -0.5 37.5 6.1
GOE 797 AIRFOIL 16.0 5.0 1.957 51.2 9.5 37.5 4.4
GOE 257 AIRFOIL 8.8 4.1 1.356 36.7 8.0 36.8 2.1
SG6050 16.0 3.2 1.471 34.3 12.5 36.8 3.1
NACA 2418 18.0 2.0 0.459 7.2 7.5 36.4 4.0