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 % Camber % Camber Chord % CL Max CD Min
<< First < Prev 42 43 44 45 46 Next > Last >>
RAE(NPL) 5212 11.92 1.827 69.13 1.408 0.0053
RAF 15 6.45 2.564 30 1.282 0.0059
RAF 19 10.52 10.065 40 2.23 0.0084
RAF 25 6.43 1.043 49.86 0.746 0.0043
RAF 26 6.58 2.13 49.9 1.016 0.0041
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.05 0.42 0.05 -0.34
0.1 0.6 0.1 -0.48
0.16 0.76 0.16 -0.59
0.24 0.94 0.24 -0.72
0.35 1.14 0.35 -0.85
0.5 1.37 0.5 -1
0.65 1.56 0.65 -1.12
0.8 1.74 0.8 -1.22
0.96 1.91 0.96 -1.32
1.5 2.4 1.5 -1.58
2.15 2.87 2.15 -1.83
3 3.34 3 -2.09
3.81 3.68 3.81 -2.29
5.9 4.32 5.9 -2.72
8.43 4.9 8.43 -3.13
11.35 5.42 11.35 -3.5
14.65 5.9 14.65 -3.84
18.28 6.3 18.28 -4.14
22.22 6.64 22.22 -4.38
26.43 6.91 26.43 -4.58
30.87 7.11 30.87 -4.69
35.49 7.23 35.49 -4.71
40.25 7.26 40.25 -4.61
45.1 7.2 45.1 -4.4
50 7.05 50 -4.05
54.9 6.79 54.9 -3.53
59.76 6.42 59.76 -2.95
64.51 5.94 64.51 -2.32
69.13 5.4 69.13 -1.73
73.57 4.81 73.57 -1.24
77.78 4.2 77.78 -0.84
81.72 3.57 81.72 -0.53
85.36 2.97 85.36 -0.31
88.65 2.4 88.65 -0.15
91.57 1.86 91.57 -0.05
94.1 1.33 94.1 0
96.19 0.86 96.19 0.01
97.85 0.46 97.85 0
99.04 0.19 99.04 0
99.76 0.04 99.76 0
100 0 100 0
V 1.0