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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 49 50 51 52 53 Next > Last >>
NACA 662-415 14.99 44.95 2.217 50 0.751 0.0001
NACA 4415 14.99 30 3.939 40 1.588 0.0058
NACA 0015 15.01 28.73 0 0 1.287 0.0064
BOEING 737 ROOT AIRFOI 15.33 19.61 0.233 4.95 1.372 0.011
KC-135 BL52.44 15.45 35 1.015 25 1.382 0.0079
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.5
0.2 1.1 0.2 -0.6
0.3 1.25 0.3 -0.8
0.31 1.21 0.69 -1.01
0.54 1.47 0.96 -1.19
1.02 1.87 1.48 -1.45
2.24 2.59 2.76 -1.85
4.71 3.72 5.29 -2.45
7.2 4.62 7.8 -2.92
9.7 5.38 10.3 -3.31
14.71 6.62 15.29 -3.93
19.74 7.58 20.26 -4.4
24.77 8.33 25.23 -4.75
29.81 8.9 30.19 -5.01
34.86 9.31 35.14 -5.19
39.9 9.57 40.1 -5.29
44.95 9.69 45.05 -5.31
50 9.66 50 -5.24
55.05 9.47 54.95 -5.09
60.09 9.1 59.91 -4.82
65.13 8.43 64.87 -4.31
70.15 7.52 69.85 -3.63
75.16 6.42 74.84 -2.84
80.16 5.19 79.84 -2
85.14 3.87 84.86 -1.18
90.1 2.52 89.9 -0.45
95.05 1.2 94.95 0.07
100 0 100 0
X Y
1 0
0.9505 0.012
0.901 0.0252
0.8514 0.0387
0.8016 0.0519
0.7516 0.0642
0.7015 0.0752
0.6513 0.0843
0.6009 0.091
0.5505 0.0947
0.5 0.0966
0.4495 0.0969
0.399 0.0957
0.3486 0.0931
0.2981 0.089
0.2477 0.0833
0.1974 0.0758
0.1471 0.0662
0.097 0.0538
0.072 0.0462
0.0471 0.0372
0.0224 0.0259
0.0102 0.0187
0.0054 0.0147
0.0031 0.0121
0.003 0.0125
0.002 0.011
0.001 0.01
0 0
0 0
0.001 -0.005
0.002 -0.006
0.003 -0.008
0.0069 -0.0101
0.0096 -0.0119
0.0148 -0.0145
0.0276 -0.0185
0.0529 -0.0245
0.078 -0.0292
0.103 -0.0331
0.1529 -0.0393
0.2026 -0.044
0.2523 -0.0475
0.3019 -0.0501
0.3514 -0.0519
0.401 -0.0529
0.4505 -0.0531
0.5 -0.0524
0.5495 -0.0509
0.5991 -0.0482
0.6487 -0.0431
0.6985 -0.0363
0.7484 -0.0284
0.7984 -0.02
0.8486 -0.0118
0.899 -0.0045
0.9495 0.0007
1 0
X Y
100 0
95.05 1.2
90.1 2.52
85.14 3.87
80.16 5.19
75.16 6.42
70.15 7.52
65.13 8.43
60.09 9.1
55.05 9.47
50 9.66
44.95 9.69
39.9 9.57
34.86 9.31
29.81 8.9
24.77 8.33
19.74 7.58
14.71 6.62
9.7 5.38
7.2 4.62
4.71 3.72
2.24 2.59
1.02 1.87
0.54 1.47
0.31 1.21
0.3 1.25
0.2 1.1
0.1 1
0 0
0 0
0.1 -0.5
0.2 -0.6
0.3 -0.8
0.69 -1.01
0.96 -1.19
1.48 -1.45
2.76 -1.85
5.29 -2.45
7.8 -2.92
10.3 -3.31
15.29 -3.93
20.26 -4.4
25.23 -4.75
30.19 -5.01
35.14 -5.19
40.1 -5.29
45.05 -5.31
50 -5.24
54.95 -5.09
59.91 -4.82
64.87 -4.31
69.85 -3.63
74.84 -2.84
79.84 -2
84.86 -1.18
89.9 -0.45
94.95 0.07
100 0
V 1.1