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 48 49 50 51 52 Next > Last >>
NACA 652-415 14.98 39.9 2.218 50 1.248 0.0026
NACA 632-415 14.98 34.85 2.213 50 1.268 0.0028
NACA 747A415 14.98 40.18 3.048 34.96 1.297 0.0076
NACA 671-215 14.98 50 1.111 50 0.803 0.0001
NACA 662-215 14.98 44.98 1.109 50 0.915 0.0002
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.9 0.1 -0.3
0.2 1 0.2 -0.5
0.3 1.2 0.3 -0.7
0.31 1.21 0.69 -1.01
0.54 1.48 0.96 -1.2
1.02 1.9 1.48 -1.47
4.7 3.86 5.3 -2.6
7.18 4.79 7.82 -3.1
9.68 5.58 10.32 -3.51
14.7 6.84 15.3 -4.15
19.73 7.81 20.27 -4.63
24.76 8.55 25.24 -4.97
29.81 9.09 30.19 -5.21
34.85 9.46 35.15 -5.34
39.9 9.64 40.1 -5.36
44.95 9.62 45.05 -5.24
50 9.37 50 -4.96
55.04 8.91 54.96 -4.53
60.08 8.26 59.92 -3.98
65.11 7.46 64.89 -3.34
70.12 6.54 69.88 -2.65
75.13 5.53 74.87 -1.95
80.13 4.45 79.87 -1.26
85.11 3.32 84.89 -0.63
90.08 2.18 89.92 -0.11
95.04 1.06 94.96 0.21
100 0 100 0
X Y
1 0
0.9504 0.0106
0.9008 0.0218
0.8511 0.0332
0.8013 0.0445
0.7513 0.0553
0.7012 0.0654
0.6511 0.0746
0.6008 0.0826
0.5504 0.0891
0.5 0.0937
0.4495 0.0962
0.399 0.0964
0.3485 0.0946
0.2981 0.0909
0.2476 0.0855
0.1973 0.0781
0.147 0.0684
0.0968 0.0558
0.0718 0.0479
0.047 0.0386
0.0102 0.019
0.0054 0.0148
0.0031 0.0121
0.003 0.012
0.002 0.01
0.001 0.009
0 0
0 0
0.001 -0.003
0.002 -0.005
0.003 -0.007
0.0069 -0.0101
0.0096 -0.012
0.0148 -0.0147
0.053 -0.026
0.0782 -0.031
0.1032 -0.0351
0.153 -0.0415
0.2027 -0.0463
0.2524 -0.0497
0.3019 -0.0521
0.3515 -0.0534
0.401 -0.0536
0.4505 -0.0524
0.5 -0.0496
0.5496 -0.0453
0.5992 -0.0398
0.6489 -0.0334
0.6988 -0.0265
0.7487 -0.0195
0.7987 -0.0126
0.8489 -0.0063
0.8992 -0.0011
0.9496 0.0021
1 0
X Y
100 0
95.04 1.06
90.08 2.18
85.11 3.32
80.13 4.45
75.13 5.53
70.12 6.54
65.11 7.46
60.08 8.26
55.04 8.91
50 9.37
44.95 9.62
39.9 9.64
34.85 9.46
29.81 9.09
24.76 8.55
19.73 7.81
14.7 6.84
9.68 5.58
7.18 4.79
4.7 3.86
1.02 1.9
0.54 1.48
0.31 1.21
0.3 1.2
0.2 1
0.1 0.9
0 0
0 0
0.1 -0.3
0.2 -0.5
0.3 -0.7
0.69 -1.01
0.96 -1.2
1.48 -1.47
5.3 -2.6
7.82 -3.1
10.32 -3.51
15.3 -4.15
20.27 -4.63
25.24 -4.97
30.19 -5.21
35.15 -5.34
40.1 -5.36
45.05 -5.24
50 -4.96
54.96 -4.53
59.92 -3.98
64.89 -3.34
69.88 -2.65
74.87 -1.95
79.87 -1.26
84.89 -0.63
89.92 -0.11
94.96 0.21
100 0
V 1.1