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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 50 51 52 53 54 Next > Last >>
P-51H ROOT 15.49 44.98 1.333 47.5 1.223 0.0031
NACA 0016 15.91 27.3202 0 0 1.332 0.0106
S8037 15.98 33.47 2.431 36.9 1.574 0.005
S8036 15.99 36.85 1.825 36.85 1.538 0.005
S8036 (16%) 16 36.848 1.821 36.848 1.538 0.0054
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.17 0.86 0.33 -0.79
0.39 1.2 0.61 -1.08
0.62 1.45 0.88 -1.29
0.87 1.66 1.13 -1.45
1.19 1.83 1.39 -1.58
1.85 2.26 2.15 -1.9
2.34 2.51 2.66 -2.07
4.82 3.56 5.18 -2.81
7.31 4.4 7.69 -3.39
12.31 5.72 12.69 -4.29
14.81 6.26 15.19 -4.64
17.32 6.74 17.68 -4.96
19.83 7.15 20.17 -5.23
22.34 7.52 22.66 -5.46
24.85 7.84 25.15 -5.67
27.37 8.12 27.64 -5.85
29.88 8.37 30.12 -6
32.39 8.57 32.61 -6.13
34.91 8.74 35.09 -6.23
37.43 8.88 37.57 -6.31
39.94 8.98 40.06 -6.37
42.46 9.04 42.54 -6.41
44.98 9.07 45.02 -6.42
47.5 9.07 47.5 -6.41
50.02 9.02 49.98 -6.37
52.54 8.94 52.46 -6.31
55.06 8.82 54.94 -6.22
57.59 8.65 57.41 -6.11
60.12 8.42 59.88 -5.95
62.65 8.11 62.35 -5.73
65.17 7.71 64.83 -5.45
67.67 7.24 67.33 -5.12
70.17 6.73 69.83 -4.74
72.67 6.18 72.33 -4.35
75.16 5.59 74.84 -3.93
77.64 4.98 77.36 -3.48
80.13 4.35 79.87 -3.03
82.61 3.71 82.39 -2.56
85.09 3.08 84.91 -2.1
87.57 2.45 87.43 -1.64
90.05 1.83 89.95 -1.2
92.53 1.25 92.47 -0.79
95.02 0.72 94.98 -0.42
97.51 0.28 97.49 -0.13
98.5 0.13 98.5 -0.05
99 0.08 99 -0.02
100 0 100 0
X Y
1 0
0.99 0.0008
0.985 0.0013
0.9751 0.0028
0.9502 0.0072
0.9253 0.0125
0.9005 0.0183
0.8757 0.0245
0.8509 0.0308
0.8261 0.0371
0.8013 0.0435
0.7764 0.0498
0.7516 0.0559
0.7267 0.0618
0.7017 0.0673
0.6767 0.0724
0.6517 0.0771
0.6265 0.0811
0.6012 0.0842
0.5759 0.0865
0.5506 0.0882
0.5254 0.0894
0.5002 0.0902
0.475 0.0907
0.4498 0.0907
0.4246 0.0904
0.3994 0.0898
0.3743 0.0888
0.3491 0.0874
0.3239 0.0857
0.2988 0.0837
0.2737 0.0812
0.2485 0.0784
0.2234 0.0752
0.1983 0.0715
0.1732 0.0674
0.1481 0.0626
0.1231 0.0572
0.0731 0.044
0.0482 0.0356
0.0234 0.0251
0.0185 0.0226
0.0119 0.0183
0.0087 0.0166
0.0062 0.0145
0.0039 0.012
0.0017 0.0086
0 0
0 0
0.0033 -0.0079
0.0061 -0.0108
0.0088 -0.0129
0.0113 -0.0145
0.0139 -0.0158
0.0215 -0.019
0.0266 -0.0207
0.0518 -0.0281
0.0769 -0.0339
0.1269 -0.0429
0.1519 -0.0464
0.1768 -0.0496
0.2017 -0.0523
0.2266 -0.0546
0.2515 -0.0567
0.2764 -0.0585
0.3012 -0.06
0.3261 -0.0613
0.3509 -0.0623
0.3757 -0.0631
0.4006 -0.0637
0.4254 -0.0641
0.4502 -0.0642
0.475 -0.0641
0.4998 -0.0637
0.5246 -0.0631
0.5494 -0.0622
0.5741 -0.0611
0.5988 -0.0595
0.6235 -0.0573
0.6483 -0.0545
0.6733 -0.0512
0.6983 -0.0474
0.7233 -0.0435
0.7484 -0.0393
0.7736 -0.0348
0.7987 -0.0303
0.8239 -0.0256
0.8491 -0.021
0.8743 -0.0164
0.8995 -0.012
0.9247 -0.0079
0.9498 -0.0042
0.9749 -0.0013
0.985 -0.0005
0.99 -0.0002
1 0
X Y
100 0
99 0.08
98.5 0.13
97.51 0.28
95.02 0.72
92.53 1.25
90.05 1.83
87.57 2.45
85.09 3.08
82.61 3.71
80.13 4.35
77.64 4.98
75.16 5.59
72.67 6.18
70.17 6.73
67.67 7.24
65.17 7.71
62.65 8.11
60.12 8.42
57.59 8.65
55.06 8.82
52.54 8.94
50.02 9.02
47.5 9.07
44.98 9.07
42.46 9.04
39.94 8.98
37.43 8.88
34.91 8.74
32.39 8.57
29.88 8.37
27.37 8.12
24.85 7.84
22.34 7.52
19.83 7.15
17.32 6.74
14.81 6.26
12.31 5.72
7.31 4.4
4.82 3.56
2.34 2.51
1.85 2.26
1.19 1.83
0.87 1.66
0.62 1.45
0.39 1.2
0.17 0.86
0 0
0 0
0.33 -0.79
0.61 -1.08
0.88 -1.29
1.13 -1.45
1.39 -1.58
2.15 -1.9
2.66 -2.07
5.18 -2.81
7.69 -3.39
12.69 -4.29
15.19 -4.64
17.68 -4.96
20.17 -5.23
22.66 -5.46
25.15 -5.67
27.64 -5.85
30.12 -6
32.61 -6.13
35.09 -6.23
37.57 -6.31
40.06 -6.37
42.54 -6.41
45.02 -6.42
47.5 -6.41
49.98 -6.37
52.46 -6.31
54.94 -6.22
57.41 -6.11
59.88 -5.95
62.35 -5.73
64.83 -5.45
67.33 -5.12
69.83 -4.74
72.33 -4.35
74.84 -3.93
77.36 -3.48
79.87 -3.03
82.39 -2.56
84.91 -2.1
87.43 -1.64
89.95 -1.2
92.47 -0.79
94.98 -0.42
97.49 -0.13
98.5 -0.05
99 -0.02
100 0
V 1.1