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 (%)
GOE 531 AIRFOIL 13.7 14.5 2.796 290.9 -0.5 21.9 5.3
GOE 462 AIRFOIL 10.8 13.3 2.381 596.0 0.0 4.7 3.7
EPPLER 420 AIRFOIL 14.3 10.7 2.477 82.8 -0.4 14.0 3.7
GOE 448 AIRFOIL 12.9 10.5 2.357 55.1 -0.5 22.5 3.7
GOE 561 AIRFOIL 24.9 10.2 2.234 40.5 -0.5 42.7 7.9
CH10 (smoothed) 12.8 10.2 2.270 69.2 -0.5 13.2 2.6
RAF 19 AIRFOIL 10.4 10.1 2.050 89.7 5.0 19.6 3.8
E423 12.5 10.0 2.357 67.7 14.5 14.1 3.2
GOE 244 (MVA PR.4) AIRFOIL 17.6 9.9 2.694 54.4 -0.5 11.4 6.2
GOE 464 AIRFOIL 7.5 9.9 2.099 392.6 0.0 9.3 3.3
FX74_CL5_140 14.0 9.9 2.231 69.1 -0.5 6.3 2.7
GOE 571 AIRFOIL 24.8 9.8 2.248 40.0 -0.5 38.6 7.6
WORTMANN FX 72-MS-150B AIRFOIL 15.0 9.7 2.116 38.9 11.0 4.8 2.6
FX 74-Cl5-140 MOD (smoothed) 13.0 9.7 2.153 84.8 3.5 7.8 2.5
GOE 525 AIRFOIL 16.4 9.7 2.712 83.1 -4.0 8.6 4.8
GOE 523 AIRFOIL 16.4 9.7 2.712 83.1 -4.0 8.6 4.8
GOE 440 AIRFOIL 15.2 9.7 1.864 117.3 0.5 12.7 2.0
SARATOV AIRFOIL 9.2 9.6 1.762 192.0 0.0 8.8 3.0
GOE 570 AIRFOIL 33.6 9.6 2.416 42.5 -0.5 49.2 10.7
Marsden 27.8 9.6 2.809 59.3 -5.5 8.6 8.8
USA 31 AIRFOIL 14.8 9.3 2.320 63.3 -0.5 23.8 4.5
USA 32 AIRFOIL 14.7 9.3 2.313 61.3 -0.5 30.9 4.5
GOE 652 AIRFOIL 16.9 9.2 2.483 61.3 -0.5 4.0 6.4
GOE 234 (MVA CA5) AIRFOIL 14.2 9.1 2.086 52.3 -0.5 21.2 3.7
EPPLER 377 (MODIFIED) AIRFOIL 3.7 9.1 1.453 103.6 9.5 3.3 1.8
EPPLER 376 AIRFOIL 2.4 8.9 1.441 132.7 4.0 2.4 1.7
GOE 482 AIRFOIL 16.4 8.8 2.297 60.0 -0.5 8.9 4.7
GOE 481 AIRFOIL 12.8 8.8 2.295 421.1 10.0 23.1 5.4
EPPLER 421 AIRFOIL 14.5 8.7 2.171 53.4 -0.1 13.8 3.5
EPPLER 377 AIRFOIL 3.8 8.7 1.609 127.2 7.0 2.8 1.8
S1223 12.1 8.7 2.425 125.4 8.0 9.0 3.2
St. CYR 234 (Bartel 17-IC) 16.0 8.6 1.873 52.5 -0.5 18.9 5.4
N-24 16.9 8.6 1.842 30.6 -0.5 35.4 5.0
S1223 RTL 13.5 8.5 2.264 140.7 5.0 10.8 3.2
GOE 243 (MVA PR.3) AIRFOIL 18.9 8.4 2.458 56.0 -0.5 13.6 6.0
GOE 241 (MVA PR.1) AIRFOIL 18.7 8.4 2.477 54.1 -0.5 18.7 5.5
WORTMANN FX 72-MS-150A AIRFOIL 15.0 8.3 1.937 58.7 -0.5 5.9 2.6
JN-153 AIRFOIL 17.6 8.3 2.047 47.1 -0.5 9.6 3.6
NACA M27 AIRFOIL 11.9 8.3 1.621 23.6 -0.5 27.6 3.0
GOE 572 AIRFOIL 18.5 8.3 1.938 41.6 -0.5 32.3 4.1
FX 72-LS-160 16.0 8.2 2.246 54.5 -0.5 7.2 3.0
NACA M26 AIRFOIL 8.2 8.2 1.351 34.0 -0.5 21.1 2.1
NACA M25 AIRFOIL 6.3 8.2 1.260 32.8 -0.5 18.6 1.8
GOE 233 (MVA CA4) AIRFOIL 11.6 8.2 1.877 69.4 -0.5 11.3 3.2
GOE 421 AIRFOIL 18.9 8.1 2.403 52.2 -0.5 28.7 5.3
Rhode St. Genese 36 16.1 8.1 1.869 47.2 -0.5 14.1 4.7
NACA M8 AIRFOIL 11.4 8.0 1.633 42.9 -0.5 7.6 3.9
GOE 226 (MVA H.36) AIRFOIL 13.9 8.0 2.021 55.0 -0.5 13.0 4.0
FX 73-CL3-152 15.2 8.0 1.979 50.1 -0.5 11.7 4.0
EPPLER 378 AIRFOIL 4.0 8.0 1.183 16.7 -0.5 2.8 1.8