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 (%)
CAP 21 (TraCFoil) 15.5 0.6 0.000 0.0 0.0 48.5 5.3
EH 3.0/12 12.0 3.0 0.045 0.3 -0.1 12.0 0.9
YS-900 9.0 0.1 0.311 11.4 5.5 9.4 0.4
NASA SC(2)-0402 2.0 0.2 0.328 15.7 3.5 6.2 0.4
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
HQ 0/7 7.0 0.0 0.475 21.5 3.0 4.8 0.8
NASA SC(2)-0404 4.0 0.5 0.495 15.1 0.5 8.6 0.6
GOE 443 5.0 0.0 0.512 24.3 3.0 6.6 2.1
GOE 444 5.6 0.0 0.515 31.8 3.5 9.1 2.1
NACA 16-006 6.0 0.0 0.524 21.5 2.5 14.4 2.1
NACA 16009 9.0 0.0 0.537 24.2 3.0 43.2 0.8
NACA 63-206 6.0 1.1 0.539 40.5 -0.5 4.4 0.8
BOEING-VERTOL VR-9 6.1 0.3 0.540 15.4 9.5 6.3 1.0
EPPLER 379 2.1 8.0 0.545 57.7 -0.5 2.5 1.2
EPPLER 874 HYDROFOIL 7.9 1.0 0.547 29.3 3.0 15.1 0.7
GOE 445 6.4 0.0 0.552 33.0 4.0 7.3 2.2
HQ 0/9 8.1 0.0 0.552 23.5 4.0 5.8 0.9
Eh 1.0/7.0 7.0 1.0 0.567 35.2 3.5 5.6 0.7
EPPLER 340 13.7 2.6 0.571 8.2 3.0 17.9 1.5
FX 66-H-60 6.0 1.7 0.572 28.5 4.5 7.2 0.7
EPPLER 904 9.0 1.3 0.577 31.0 2.5 14.2 0.6
LWK 80-080 8.1 0.0 0.580 35.8 3.5 29.3 0.9
HT08 5.0 0.0 0.581 11.9 3.0 16.3 0.6
NACA 0008-34 8.0 0.0 0.586 23.2 3.0 14.2 2.2
HT12 5.0 0.0 0.588 12.1 3.5 3.5 0.6
HT05 4.8 0.0 0.590 12.6 3.0 20.7 0.6
NACA 64-008A 8.0 0.0 0.599 11.7 1.5 9.8 0.9
R140 (original) 12.0 0.5 0.600 31.6 3.0 15.7 1.1
YS-915 9.1 1.8 0.612 35.6 -0.5 7.4 0.6
GOE 9K 2.5 0.9 0.612 59.1 4.5 3.4 3.8
E184 (8.33%) 8.3 1.2 0.616 21.5 6.0 6.3 1.6
E184 (8.33%) 8.3 1.2 0.616 21.5 6.0 4.8 1.6
NACA 0006 6.0 0.0 0.617 17.8 2.5 8.3 2.3
NACA 66-206 6.0 1.1 0.620 23.8 8.0 7.6 0.7
EPPLER 297 11.4 0.0 0.625 39.2 4.5 9.9 0.4
EH 0.0/9.0 9.0 0.0 0.627 30.8 4.5 7.4 1.0
S1010 HPV 6.0 0.0 0.627 30.8 5.0 5.3 1.5
NACA 65-206 6.0 1.1 0.627 22.9 1.0 5.8 0.7
S1010 HPV airfoil 6.0 0.0 0.627 30.8 5.0 7.2 1.5
MH 22 7.2% 7.2 1.8 0.635 54.9 4.5 6.8 0.3
EH 2.0/7.0 7.0 2.0 0.635 53.6 4.5 5.6 0.7
MH 22 7.2% 7.2 1.8 0.635 54.9 4.5 5.9 0.3
E230 (9.96%) 10.0 0.0 0.636 29.0 6.0 10.0 1.9
E230 (9.96%) 10.0 0.1 0.636 29.0 6.0 7.4 1.9
NACA 64-206 6.0 1.1 0.639 23.4 8.5 4.8 0.7
MH 112 10.01% 10.0 1.2 0.640 15.4 5.5 177.4 0.6
NACA 0010-35 10.0 0.0 0.643 20.1 3.0 23.7 2.3
ONERA OA206 6.0 0.8 0.643 28.2 4.5 4.9 0.6
NACA-M1 6.2 0.0 0.644 11.3 1.5 10.4 2.3