Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 39 40 41 42 43 Next > Last >>
NACA M12 11.9 30 1.942 30 1.382 0.01
NACA M20 8.26 30 5.939 30 1.436 0.0096
NACA M6 12 30 2.142 30 1.34 0.0119
NACA6451.COR 13.94 38.2 2.651 51.68 1.258 0.0029
NASA/AMES A-01 10.25 30 1.368 15 1.159 0.0144
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 2.03 1.25 -1.64
2.5 2.86 2.5 -2.13
5 4.03 5 -2.71
7.5 4.9 7.5 -3.05
10 5.61 10 -3.29
15 6.66 15 -3.57
20 7.34 20 -3.76
30 8.01 30 -3.92
40 7.94 40 -3.88
50 7.35 50 -3.72
60 6.39 60 -3.38
70 5.12 70 -2.86
80 3.66 80 -2.15
90 2.07 90 -1.19
95 1.26 95 -0.62
100 0.4 100 0
X Y
1 0.004
0.95 0.0126
0.9 0.0207
0.8 0.0366
0.7 0.0512
0.6 0.0639
0.5 0.0735
0.4 0.0794
0.3 0.0801
0.2 0.0734
0.15 0.0666
0.1 0.0561
0.075 0.049
0.05 0.0403
0.025 0.0286
0.0125 0.0203
0 0
0 0
0.0125 -0.0164
0.025 -0.0213
0.05 -0.0271
0.075 -0.0305
0.1 -0.0329
0.15 -0.0357
0.2 -0.0376
0.3 -0.0392
0.4 -0.0388
0.5 -0.0372
0.6 -0.0338
0.7 -0.0286
0.8 -0.0215
0.9 -0.0119
0.95 -0.0062
1 0
X Y
100 0.4
95 1.26
90 2.07
80 3.66
70 5.12
60 6.39
50 7.35
40 7.94
30 8.01
20 7.34
15 6.66
10 5.61
7.5 4.9
5 4.03
2.5 2.86
1.25 2.03
0 0
0 0
1.25 -1.64
2.5 -2.13
5 -2.71
7.5 -3.05
10 -3.29
15 -3.57
20 -3.76
30 -3.92
40 -3.88
50 -3.72
60 -3.38
70 -2.86
80 -2.15
90 -1.19
95 -0.62
100 0
V 1.1