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 38 39 40 41 42 Next > Last >>
NACA 663-418 17.98 44.94 2.216 50 1.394 0.0076
NACA 664-221 20.98 44.97 1.119 50 1.434 0.008
NACA 671-215 14.98 50 1.111 50 0.803 0.0001
NACA 747A315 14.97 40.2 2.531 35 1.2 0.0102
NACA 747A415 14.98 40.18 3.048 34.96 1.297 0.0076
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.35
0.2 1.2 0.2 -0.6
0.28 1.41 0.72 -1.21
0.51 1.69 0.99 -1.41
0.98 2.15 1.52 -1.72
2.19 3 2.81 -2.26
4.66 4.31 5.34 -3.04
7.14 5.35 7.86 -3.65
9.64 6.23 10.36 -4.16
14.65 7.67 15.35 -4.98
19.68 8.77 20.32 -5.59
24.73 9.63 25.27 -6.05
29.78 10.29 30.23 -6.4
34.83 10.76 35.17 -6.64
39.89 11.06 40.12 -6.78
44.94 11.19 45.06 -6.81
50 11.15 50 -6.74
55.06 10.92 54.94 -6.54
60.11 10.46 59.89 -6.18
65.15 9.64 64.85 -5.52
70.18 8.54 69.82 -4.65
75.19 7.24 74.81 -3.66
80.19 5.79 79.82 -2.61
85.16 4.28 84.84 -1.58
90.12 2.74 89.88 -0.68
95.06 1.28 94.94 -0.01
100 0 100 0
X Y
1 0
0.9506 0.0128
0.9012 0.0274
0.8516 0.0428
0.8019 0.0579
0.7519 0.0724
0.7018 0.0854
0.6515 0.0964
0.6011 0.1046
0.5506 0.1092
0.5 0.1115
0.4494 0.1119
0.3989 0.1106
0.3483 0.1076
0.2978 0.1029
0.2473 0.0963
0.1968 0.0877
0.1465 0.0767
0.0964 0.0623
0.0714 0.0535
0.0466 0.0431
0.0219 0.03
0.0098 0.0215
0.0051 0.0169
0.0028 0.0141
0.002 0.012
0.001 0.01
0 0
0 0
0.001 -0.0035
0.002 -0.006
0.0072 -0.0121
0.0099 -0.0141
0.0152 -0.0172
0.0281 -0.0226
0.0534 -0.0304
0.0786 -0.0365
0.1036 -0.0416
0.1535 -0.0498
0.2032 -0.0559
0.2527 -0.0605
0.3023 -0.064
0.3517 -0.0664
0.4012 -0.0678
0.4506 -0.0681
0.5 -0.0674
0.5494 -0.0654
0.5989 -0.0618
0.6485 -0.0552
0.6982 -0.0465
0.7481 -0.0366
0.7982 -0.0261
0.8484 -0.0158
0.8988 -0.0068
0.9494 -0.0001
1 0
X Y
100 0
95.06 1.28
90.12 2.74
85.16 4.28
80.19 5.79
75.19 7.24
70.18 8.54
65.15 9.64
60.11 10.46
55.06 10.92
50 11.15
44.94 11.19
39.89 11.06
34.83 10.76
29.78 10.29
24.73 9.63
19.68 8.77
14.65 7.67
9.64 6.23
7.14 5.35
4.66 4.31
2.19 3
0.98 2.15
0.51 1.69
0.28 1.41
0.2 1.2
0.1 1
0 0
0 0
0.1 -0.35
0.2 -0.6
0.72 -1.21
0.99 -1.41
1.52 -1.72
2.81 -2.26
5.34 -3.04
7.86 -3.65
10.36 -4.16
15.35 -4.98
20.32 -5.59
25.27 -6.05
30.23 -6.4
35.17 -6.64
40.12 -6.78
45.06 -6.81
50 -6.74
54.94 -6.54
59.89 -6.18
64.85 -5.52
69.82 -4.65
74.81 -3.66
79.82 -2.61
84.84 -1.58
89.88 -0.68
94.94 -0.01
100 0
V 1.1