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 2 3 4 5 6 Next > Last >>
EPPLER 1200 16.93 3.48 40.77 1.818 0.0072
P-51D ROOT (BL17.5) 16.45 1.266 68.267 1.482 0.0063
S8036 (16%) 16 1.821 36.848 1.538 0.0054
S8036 15.99 1.825 36.85 1.538 0.005
S8037 15.98 2.431 36.9 1.574 0.005
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.13 0.72 0.5 -1.06
1.59 3.1 1.61 -1.77
2.93 4.33 3.27 -2.43
4.67 5.53 5.44 -3.03
6.81 6.68 8.1 -3.56
9.34 7.74 11.22 -4.01
12.24 8.69 14.77 -4.38
15.5 9.52 18.7 -4.68
19.1 10.23 22.97 -4.9
23.01 10.81 27.52 -5.06
27.18 11.28 32.3 -5.13
31.56 11.61 37.24 -5.12
36.11 11.81 42.29 -5.01
40.77 11.86 47.38 -4.8
45.49 11.77 52.48 -4.44
50.21 11.5 57.57 -3.92
54.91 11.05 62.65 -3.26
59.55 10.39 67.71 -2.49
64.14 9.54 72.73 -1.72
68.69 8.51 77.62 -1.01
73.16 7.39 82.28 -0.43
77.51 6.25 86.6 0
81.65 5.14 90.47 0.25
85.53 4.08 93.8 0.35
89.07 3.12 96.49 0.3
92.19 2.27 98.44 0.18
94.84 1.54 99.61 0.05
100 0 100 0
V 1.0