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Name
Begins with
OR
contains
AND
Maximum Lift (C
L
)
between
and
(at Re=100,000)
Maximum Lift-to-drag (L/D)
between
and
Thickness
between
and
Camber
between
and
Maximum number to show:
50
100
500
all
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 77-W-270
27.0
4.3
0.283
2.1
-0.5
70.7
6.1
YS-900
9.0
0.0
0.311
11.6
5.5
19.8
1.5
NASA SC(2)-0402 AIRFOIL
2.0
0.2
0.328
20.2
3.5
5.1
1.3
NASA SC(2)-0403 AIRFOIL
3.0
0.4
0.408
19.4
5.0
6.3
1.3
NACA 2415
15.0
2.0
0.410
7.4
8.0
30.2
3.3
NASA SC(2)-0503 AIRFOIL
3.0
0.2
0.435
23.9
4.5
6.5
1.3
NACA 23021
21.0
2.4
0.443
6.6
7.5
44.5
4.9
NACA 2418
18.0
2.0
0.459
7.2
7.5
36.4
4.0
HQ 0/7 AIRFOIL
7.0
0.0
0.475
29.5
3.0
5.0
1.6
NASA SC(2)-0404 AIRFOIL
4.0
0.5
0.495
18.5
6.0
7.4
1.4
NACA 2421
21.0
2.0
0.501
7.3
7.5
42.4
4.7
GOE 443 AIRFOIL
5.0
0.0
0.512
30.1
3.0
7.4
1.5
GOE 444 AIRFOIL
5.6
0.0
0.515
31.6
3.5
10.3
1.5
NACA 16-006
6.0
0.0
0.524
23.3
2.5
17.4
1.5
NACA 16009
9.0
0.0
0.537
23.3
3.0
26.4
1.6
NACA 63-206
6.0
1.1
0.539
19.0
-0.5
3.2
1.5
BOEING-VERTOL VR-9 AIRFOIL
6.0
0.3
0.540
15.8
9.5
6.3
1.6
EPPLER 379 AIRFOIL
2.2
8.0
0.545
73.3
-0.5
2.8
1.7
EPPLER 874 HYDROFOIL AIRFOIL
7.9
1.0
0.547
33.1
3.0
15.1
1.7
GOE 445 AIRFOIL
6.4
0.0
0.552
40.2
4.0
10.3
1.6
HQ 0/9 AIRFOIL
8.1
0.0
0.552
34.0
4.0
5.8
1.8
Eh 1.0/7.0
7.0
1.0
0.567
41.2
3.5
5.7
1.6
EPPLER 340 AIRFOIL
13.7
2.6
0.571
10.1
3.0
15.0
2.5
FX 66-H-60
6.0
1.7
0.572
40.3
4.5
7.2
1.6
EPPLER 904 AIRFOIL
9.0
1.3
0.577
42.1
2.5
14.1
1.6
LWK 80-080
8.1
0.0
0.580
34.4
3.5
12.0
1.7
HT08
5.0
0.0
0.581
19.3
3.0
12.7
1.7
NACA 0008-34
8.0
0.0
0.586
26.2
3.0
17.4
1.7
HT12
5.0
0.0
0.588
23.8
3.5
8.9
1.7
HT05
4.8
0.0
0.590
18.0
2.5
16.8
1.7
NACA 64-008A AIRFOIL
8.0
0.0
0.599
13.7
1.5
10.4
1.7
R140 (original)
12.0
0.4
0.600
34.1
3.0
17.1
1.9
GOE 9K AIRFOIL
2.4
0.9
0.611
71.3
4.5
7.3
1.4
YS-915
9.1
1.8
0.612
34.0
-0.5
15.0
1.6
E184 (8.33%)
8.3
1.2
0.616
34.3
6.0
5.5
1.8
NACA 0006
6.0
0.0
0.616
21.4
2.5
10.6
1.8
NACA 66-206
6.0
1.1
0.620
26.8
8.0
6.0
1.5
EPPLER 297 AIRFOIL
11.3
0.0
0.625
50.8
4.5
7.2
2.0
NACA 65-206
6.0
1.1
0.627
26.3
1.0
4.5
1.5
EH 0.0/9.0
9.0
0.0
0.627
37.7
4.5
7.4
1.9
S1010 HPV airfoil
6.0
0.0
0.627
39.4
5.0
6.2
1.9
EH 2.0/7.0
7.0
2.0
0.635
54.8
4.5
5.7
1.6
MH 22 7.2%
7.2
1.8
0.635
64.1
4.5
6.6
1.7
E230 (9.96%)
10.0
0.0
0.636
33.9
6.0
8.6
2.2
NACA 64-206
6.0
1.1
0.639
26.8
0.5
3.6
1.5
NACA 0010-35
10.0
0.0
0.642
20.9
3.0
28.6
1.8
ONERA OA206 AIRFOIL
6.0
0.8
0.643
31.2
4.5
7.1
1.6
NACA-M1 AIRFOIL
6.2
0.0
0.644
12.4
1.5
17.4
1.9
GOE 780 AIRFOIL
11.9
1.0
0.649
31.4
0.5
22.6
1.8
NASA SC(2)-0406 AIRFOIL
6.0
0.3
0.664
21.6
2.0
10.4
1.6