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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 3 4 5 6 7 Next > Last >>
NACA 632-415 14.98 34.85 2.213 50 1.268 0.0028
NACA 4412 12.02 30 3.943 40 1.649 0.0029
NACA6451.COR 13.94 38.2 2.651 51.68 1.258 0.0029
P-51H ROOT 15.49 44.98 1.333 47.5 1.223 0.0031
S7012 8.75 27.74 1.963 38.07 1.024 0.0032
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.5
0.2 1.2 0.2 -0.6
0.3 1.29 0.7 -1.09
0.53 1.59 0.98 -1.31
0.99 2.07 1.51 -1.65
2.2 2.96 2.8 -2.22
4.66 4.26 5.34 -3
7.15 5.26 7.85 -3.57
9.65 6.08 10.35 -4.01
14.67 7.35 15.33 -4.66
19.71 8.28 20.3 -5.1
24.75 8.94 25.25 -5.36
29.8 9.36 30.2 -5.47
34.85 9.56 35.15 -5.44
39.91 9.53 40.1 -5.24
44.96 9.29 45.05 -4.91
50 8.87 50 -4.46
55.04 8.3 54.96 -3.92
60.07 7.6 59.93 -3.31
65.09 6.78 64.91 -2.66
70.11 5.88 69.89 -1.99
75.11 4.91 74.89 -1.33
80.1 3.9 79.9 -0.72
85.08 2.89 84.92 -0.19
90.06 1.88 89.94 0.18
95.03 0.93 94.97 0.33
100 0 100 0
X Y
1 0
0.9503 0.0093
0.9006 0.0188
0.8508 0.0289
0.801 0.039
0.7511 0.0491
0.7011 0.0588
0.6509 0.0678
0.6007 0.076
0.5504 0.083
0.5 0.0887
0.4496 0.0929
0.3991 0.0953
0.3485 0.0956
0.298 0.0936
0.2475 0.0894
0.1971 0.0828
0.1467 0.0735
0.0965 0.0608
0.0715 0.0526
0.0466 0.0426
0.022 0.0296
0.0099 0.0207
0.0053 0.0159
0.003 0.0129
0.002 0.012
0.001 0.01
0 0
0 0
0.001 -0.005
0.002 -0.006
0.007 -0.0109
0.0098 -0.0131
0.0151 -0.0165
0.028 -0.0222
0.0534 -0.03
0.0785 -0.0357
0.1035 -0.0401
0.1533 -0.0466
0.203 -0.051
0.2525 -0.0536
0.302 -0.0547
0.3515 -0.0544
0.401 -0.0524
0.4505 -0.0491
0.5 -0.0446
0.5496 -0.0392
0.5993 -0.0331
0.6491 -0.0266
0.6989 -0.0199
0.7489 -0.0133
0.799 -0.0072
0.8492 -0.0019
0.8994 0.0018
0.9497 0.0033
1 0
X Y
100 0
95.03 0.93
90.06 1.88
85.08 2.89
80.1 3.9
75.11 4.91
70.11 5.88
65.09 6.78
60.07 7.6
55.04 8.3
50 8.87
44.96 9.29
39.91 9.53
34.85 9.56
29.8 9.36
24.75 8.94
19.71 8.28
14.67 7.35
9.65 6.08
7.15 5.26
4.66 4.26
2.2 2.96
0.99 2.07
0.53 1.59
0.3 1.29
0.2 1.2
0.1 1
0 0
0 0
0.1 -0.5
0.2 -0.6
0.7 -1.09
0.98 -1.31
1.51 -1.65
2.8 -2.22
5.34 -3
7.85 -3.57
10.35 -4.01
15.33 -4.66
20.3 -5.1
25.25 -5.36
30.2 -5.47
35.15 -5.44
40.1 -5.24
45.05 -4.91
50 -4.46
54.96 -3.92
59.93 -3.31
64.91 -2.66
69.89 -1.99
74.89 -1.33
79.9 -0.72
84.92 -0.19
89.94 0.18
94.97 0.33
100 0
V 1.1